Calculators Created by Maiarutselvan V

Verified Area of Composite Wall of 2 Layers

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Verified Inner Surface Temperature of Composite Wall for 2 Layers in Series

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Verified Thermal Resistance of Composite Wall with 2 Layers in Series

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5 More 2 Layers Calculators

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Verified Area of Composite Wall of 3 Layers

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Verified Inner Surface Temperature of Composite Wall of 3 Layers in Series

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Verified Length of 3rd Layer of Composite Wall in Conduction through Walls

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Verified Thermal Resistance of Composite Wall with 3 Layers in Series

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2 More 3 Layers Calculators

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Verified Aerodynamic Heating to Surface

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Verified Chapman-Rubesin Factor

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Verified Coefficient of Friction using Stanton Equation for Incompressible Flow

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Verified Density Calculation using Chapman-Rubesin Factor

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Verified Stanton Number for Incompressible Flow

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Verified Static Density Calculation using Chapman-Rubesin Factor

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Verified Static Viscosity Calculation using Chapman-Rubesin Factor

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Verified Thermal Conductivity using Prandtl Number

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Verified Viscosity Calculation using Chapman-Rubesin Factor

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7 More Aero Thermal Dynamics Calculators

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Verified Airspeed Measurement by Venturi

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Verified Dynamic Pressure in Incompressible Flow

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Verified Test Section Velocity by Manometric Height for Wind Tunnel

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Verified Total Pressure in Incompressible Flow

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Verified Wind Tunnel Pressure Difference by Manometer

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Verified Wind Tunnel Test Section Velocity

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4 More Aerodynamic Measurements and Wind Tunnel Testing Calculators

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Verified Sideslip Angle for Aircraft

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10 More Aerodynamic Parameters Calculators

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Verified Normal Force Coefficient with Aerodynamic Normal Force

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Verified Rolling Moment

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Verified Rolling moment coefficient

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Verified Velocity along Pitch Axis for Small Sideslip Angle

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Verified Velocity along Roll Axis for Small Angle of Attack

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13 More Aircraft Dynamics Nomenclature Calculators

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Verified Current Gain of Amplifier in Decibels

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20 More Amplifier Characteristics Calculators

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Verified Non-Dimensional Pressure

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Verified Non-Dimensional Pressure for High Mach Number

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Verified Slenderness Ratio with Cone Radius for Hypersonic Vehicle

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8 More Approximate Methods of Hypersonic Inviscid Flowfields Calculators

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Verified Coefficient of Drag over Flat under Freestream Flow Conditions

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Verified Drag Force over Flat Plate

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Verified Freestream Stanton Number for Flat Plate

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Verified Local Heat Transfer over Flat Plate using Stanton Number

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Verified Pressure Ratio for Insulated Flat Plate, Weak Interaction

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10 More Approximate Results Applied to Hypersonic Vehicles Calculators

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Verified Pressure Coefficient for Blast Wave Theory

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5 More Blast Wave Part Theory Calculators

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Verified Coefficient of Friction given Frictional Force

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Verified Frictional Force

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5 More Body Lying on Rough Inclined Plane Calculators

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Verified Acceleration of System given Mass of Body A

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Verified Acceleration of System given Mass of Body B

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Verified Frictional Force on Body B

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Verified Tension in String given Mass of Body A

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Verified Tension in String given Mass of Body B

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1 More Body Lying on Rough Inclined Plane Calculators

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Verified Tension in String when One Body is Lying on Smooth Inclined Plane

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3 More Body Lying on Smooth Inclined Plane Calculators

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Verified Angle of Inclination of Plane with Body A

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Verified Angle of Inclination of Plane with Body B

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2 More Body Lying on Smooth Inclined Plane Calculators

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Created Area of Surface for Average Drag Coefficient

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Created Average Coefficient of Drag for Drag Force

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Created Coefficient of Drag for Blasius's Solution

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Created Coefficient of Drag for Reynold Number

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Created Distance from Leading Edge

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Created Distance from Leading Edge for Blasius's Solution

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Created Drag Force for Average Drag Coefficient

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Created Drag Force on Plate

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Created Freestream Velocity for Local Drag Coefficient

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Created Length of Plate for Reynold Number

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Created Local Drag Coefficient for Shear Stress

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Created Reynold Number at End of Plate

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Created Reynold Number for Drag Coefficient in Blasius's Solution

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Created Reynold Number for Drag Force on Plate

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Created Shear Stress at Boundary for Turbulent Boundary Layer over Flat Plate

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Created Shear Stress for Local Drag Coefficient

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Created Thickness of Boundary Layer

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Created Thickness of Boundary Layer for Blasius's Solution

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Created Velocity of Fluid for Reynold Number

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Created Viscosity of Liquid for Drag Force on Plate

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Created Width of Plate for Drag Force on Plate

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Created Angle of heel for metacentric height in experimental method

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Created Centre of Buoyancy

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Created Meta-centric height for time period of oscillation and radius of gyration

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Created Meta-centric height in experimental method

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Created Movable weight for metacentric height in experimental method

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Created Radius of gyration for metacentric height and time period of oscillation

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Created Time Period of Oscillation of Ship

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Created Volume of body in fluid for metacentric height and BG

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Created Volume of fluid displaced

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2 More Buoyancy Calculators

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Verified Thrust available for given excess power

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15 More Climbing Flight Calculators

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Created Bulk Modulus for Velocity of Sound Wave

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Created Mach Angle for Compressible Fluid Flow

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Created Mach Number for Compressible Fluid Flow

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Created Pressure Ratio for Maximum Flow Rate through Nozzle

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Created Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid

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Created Velocity of Projectile of Mach Cone in Compressible Fluid Flow

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Created Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow

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Created Velocity of Sound Wave given Bulk Modulus

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Created Velocity of Sound Wave given Mach Number for Compressible Fluid Flow

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1 More Compressible Flow Parameters Calculators

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Verified Emissivity

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Verified Reference Viscosity

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9 More Computational Fluid Dynamic Solutions Calculators

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Verified Convection Resistance for Cylindrical Layer

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Verified Length of Cylindrical Wall for given Heat Flow Rate

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14 More Conduction in Cylinder Calculators

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Verified Convection Resistance for Spherical Layer

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Verified Heat Flow Rate through Spherical Composite Wall of 2 Layers in Series

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Verified Inner Surface Temperature of Spherical Wall

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Verified Outer Surface Temperature of Spherical Wall

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Verified Thermal Resistance of Spherical Composite Wall of 2 Layers in Series with Convection

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Verified Thickness of Spherical Wall to Maintain given Temperature Difference

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Verified Total Thermal Resistance of Spherical Wall of 2 Layers without Convection

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Verified Total Thermal Resistance of Spherical wall of 3 Layers without Convection

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Verified Total Thermal Resistance of Spherical Wall with Convection on Both Side

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2 More Conduction in Sphere Calculators

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Created Cutting Force for Frictional Force along Tool Rake Face and Thrust Force

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Created Cutting Force given Shear Force and Thrust Force

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4 More Cutting Force Calculators

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Created Circulation for Lift Force on Cylinder

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Created Length of Cylinder for Lift Force on Cylinder

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Created Location of Stagnation points for Rotating Cylinder in Uniform Flow Field

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Created Radius of Cylinder for location of Stagnation Points

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Created Radius of Cylinder for Single Stagnation Point

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2 More Cylinder Properties Calculators

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Verified Simplified Pressure Ratio for Blunt Cylinder Blast Wave

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7 More Cylindrical Blast Wave Calculators

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Verified Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number

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Verified Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number

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2 More Dimensionless Quantities Calculators

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Created Diameter of Pipe for Difference in Pressure in Viscous Flow

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Created Diameter of Pipe for Head Loss due to Friction in Viscous Flow

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Created Diameter of Pipe for Loss of Pressure Head in Viscous Flow

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Created Diameter of Pipe from Maximum Velocity and Velocity at Any Radius

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Created Diameter of Shaft for Speed and Shear Stress of Fluid in Journal Bearing

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Created Diameter of Shaft for Torque Required in Foot-Step Bearing

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Created Diameter of Sphere in Falling Sphere Resistance Method

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Created External or Outer Radius of Collar for Total Torque

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Created Internal or Inner Radius of Collar for Total Torque

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Created Length for Difference of Pressure in Viscous Flow between Two Parallel Plates

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Created Length for Pressure Head Loss in Viscous Flow between Two Parallel Plates

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Created Length of Pipe for Difference of Pressure in Viscous Flow

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Created Length of Pipe for Head Loss due to Friction in Viscous Flow

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Created Length of Pipe for Loss of Pressure Head in Viscous Flow

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Created Length of Tube in Capillary Tube Method

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Created Radius of Capillary Tube

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Created Thickness of Oil Film for Shear Force in Journal Bearing

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Created Thickness of Oil Film for Speed and Diameter of Shaft in Journal Bearing

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Created Thickness of Oil Film for Torque required in Foot-Step Bearing

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Created Coefficient of Discharge for Time Required to Empty Reservoir

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Created Discharge over Broad-Crested Weir

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Created Discharge over Broad-Crested Weir for Head of Liquid at Middle

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Created Discharge over Broad-Crested Weir with Velocity of Approach

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Created Discharge over Rectangle Notch or Weir

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Created Discharge over Rectangle Weir Considering Bazin's formula

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Created Discharge over Rectangle Weir Considering Francis's formula

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Created Discharge over Rectangle Weir for Bazin's formula with Velocity of Approach

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Created Discharge over Rectangle Weir with Two End Contractions

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Created Discharge over Trapezoidal Notch or Weir

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Created Discharge over Triangular Notch or Weir

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Created Discharge with Velocity of Approach

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Created Discharge without Velocity of Approach

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Created Head of Liquid above V-notch

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Created Head of Liquid at Crest

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Created Time Required to Empty Reservoir

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Created Time Required to Empty Tank with Triangular Weir or Notch

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Verified Stream Function for 2-D Doublet Flow

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1 More Doublet Flow Calculators

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Verified Density behind Normal Shock given Upstream Density and Mach Number

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Verified Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number

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Verified Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number

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Verified Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number

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11 More Downstream Shock Waves Calculators

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Created Area of body for Lift Force in body moving on Fluid

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Created Coefficient of drag for sphere in Oseen formula when Reynolds number is between 0.2 and 5

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Created Coefficient of drag for sphere in stoke's law when Reynolds number is less than 0.2

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Created Drag Force for body moving in Fluid of Certain Density

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Created Pressure Drag from Total Drag Force on Sphere

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Created Skin Friction Drag from Total Drag Force on Sphere

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Created Total Drag force on Sphere

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4 More Drag and Forces Calculators

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Verified Emissivity per Unit Mole

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Verified Kinetic Energy per Mole

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Verified Kinetic Energy per Mole using Molar Volume

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Verified Kinetic Energy per Mole using Temperature of Gas

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Verified Mean Free Path of Single-Species Gas

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Verified Pressure using Kinetic Energy per Mole

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Verified Pressure using Molar Volume

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Verified Specific Gas Constant using Kinetic Energy per Mole

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Verified Temperature of Gas using Emissivity per Unit Mole

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Verified Temperature of Gas using Kinetic Energy per Mole

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5 More Elements of Kinetic Theory Calculators

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Verified Forward Mach Angle of Expansion Fan

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Verified Pressure Ratio across Expansion Fan

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Verified Temperature Ratio across Expansion Fan

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7 More Expansion Waves Calculators

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Created Difference of Pressure for Viscous Flow between Two Parallel Plates

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Created Difference of Pressure for Viscous or Laminar Flow

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Created Loss of Head Due to Friction

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Created Loss of Pressure Head for Viscous Flow between Two Parallel Plates

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Created Loss of Pressure Head for Viscous Flow through Circular Pipe

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Created Power Absorbed in Collar Bearing

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Created Power Absorbed in Foot-Step Bearing

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Created Power Absorbed in Overcoming Viscous Resistance in Journal Bearing

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Created Viscosity of Fluid or Oil for Capillary Tube Method

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Created Viscosity of Fluid or Oil for Movement of Piston in Dash-Pot

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Created Viscosity of Fluid or Oil in Falling Sphere Resistance Method

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Created Viscosity of Fluid or Oil in Rotating Cylinder Method

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1 More Flow Analysis Calculators

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Created Absolute pressure head at constant head and atmospheric pressure head

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Created Atmospheric pressure head at constant head and absolute pressure head

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Created Head of Liquid above Centre of Orifice

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Created Head of liquid for head loss and coefficient of velocity

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Created Loss of head due to fluid resistance

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Created Loss of head due to sudden enlargement

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Created Area of Flow for Circular Channel

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Created Bazin's constant

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Created Chezy's constant considering Bazin formula

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Created Chezy's constant considering Kutter's formula

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Created Chezy's constant considering Manning's formula

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Created Chezy's constant considering velocity

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Created Critical depth considering flow in open channels

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Created Critical depth considering minimum specific energy

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Created Critical Depth using Critical Velocity

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Created Critical velocity considering flow in open channels

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Created Discharge per unit width considering flow in open channels

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Created Hydraulic mean depth considering Bazin formula

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Created Hydraulic mean depth considering Manning's formula

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Created Hydraulic mean depth using Chezy's formula

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Created Manning's coefficient or constant

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Created Minimum Specific Energy using Critical Depth

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Created Radius of Circular Channel using Wetted Perimeter

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Created Velocity of Chezy's formula

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Created Wetted Perimeter for Circular Channel

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Verified Boundary Layer Thickness for Laminar Flow

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Verified Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory

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6 More Flow over Airfoils Calculators

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Created Coefficient of discharge

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Created Coefficient of discharge for area and velocity

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Created Coefficient of Discharge given Time for Emptying Tank

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Created Coefficient of Discharge given Time of Emptying Circular Horizontal Tank

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Created Coefficient of Discharge given Time of Emptying Hemispherical Tank

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Created Discharge in Borda's Mouthpiece Running Free

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Created Discharge in Borda's Mouthpiece Running Full

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Created Discharge in Convergent-Divergent Mouthpiece

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Created Discharge through fully sub-merged orifice

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Created Discharge through large rectangular orifice

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Created Discharge through partially sub-merged orifice

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Created Coefficient of contraction for sudden contraction

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Created Discharge in Equivalent Pipe

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Created Retarding force for gradual closure of valves

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Created Time required to close Valve for Gradual Closure of Valves

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Created Time taken by pressure wave to travel

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Created Velocity at Outlet for Head Loss at Exit of Pipe

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Created Velocity at section 1-1 for sudden enlargement

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Created Velocity at section 2-2 for sudden contraction

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Created Velocity at section 2-2 for sudden enlargement

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Created Velocity of Flow at Outlet of Nozzle

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Created Velocity of Flow at outlet of Nozzle for Efficiency and Head

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Created Velocity of Fluid for Head Loss due to Obstruction in Pipe

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Created Velocity of fluid in pipe for head loss at entrance of pipe

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Created Velocity of liquid at vena-contracta

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3 More Flow Regime Calculators

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Created Angular Speed of Outer Cylinder in Rotating Cylinder Method

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Created Buoyant Force in Falling Sphere Resistance Method

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Created Density of Fluid in Falling Sphere Resistance Method

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Created Discharge in Capillary Tube Method

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Created Drag Force in Falling Sphere Resistance Method

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Created Maximum Velocity at any Radius using Velocity

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Created Rotational Speed considering Power Absorbed and Torque in Journal Bearing

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Created Rotational Speed for Torque Required in Collar Bearing

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Created Rotational Speed for Torque Required in Foot-Step Bearing

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Created Shear Force for Torque and Diameter of Shaft in Journal Bearing

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Created Shear Force or Viscous Resistance in Journal Bearing

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Created Shear Stress in Fluid or Oil of Journal Bearing

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Created Speed of Rotation for Shear Force in Journal Bearing

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Created Torque Required Considering Power Absorbed in Journal Bearing

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Created Torque Required to Overcome Shear Force in Journal Bearing

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Created Torque Required to Overcome Viscous Resistance in Collar Bearing

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Created Torque Required to Overcome Viscous Resistance in Foot-Step Bearing

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Created Total Torque Measured by Strain in Rotating Cylinder Method

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Created Velocity at Any Radius given Radius of Pipe, and Maximum Velocity

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Created Velocity of Piston or Body for Movement of Piston in Dash-Pot

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Created Velocity of Sphere in Falling Sphere Resistance Method

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Created Freestream Velocity for Lift Coefficient in Rotating Cylinder with Circulation

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Created Freestream velocity for lift coefficient with tangential speed

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Created Freestream Velocity for single Stagnation Point

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Created Tangential velocity for single stagnation point

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5 More Fluid Parameters and Characteristics Calculators

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Created Force along shear force for given force normal to shear force, shear, friction and normal rake angle

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Created Force along Shear Force given Cutting Force and Thrust Force

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1 More Force Along Shear Calculators

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Created Force normal to shear force for given cutting force, thrust force, and shear angle

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3 More Force Normal to Shear Calculators

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Created Frictional force along tool rake face for given cutting and thrust forces, normal rake angle

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5 More Forces and Friction Calculators

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Created Length of Crest of Weir or Notch

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Created Length of Section for Discharge over Rectangle Notch or Weir

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Created Length of Weir Considering Bazin's formula with Velocity of Approach

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Created Length of Weir Considering Bazin's formula without Velocity of Approach

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Created Length of Weir Considering Francis's formula

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Created Length of Weir for Broad-Crested Weir and Head of Liquid at Middle

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Created Length of Weir for Broad-Crested Weir with Velocity of Approach

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Created Length of Weir for Discharge over Broad-Crested Weir

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Created Length of Weir or Notch for Velocity of Approach

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Created Length of Weir or Notch without Velocity of Approach

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Created Area at vena contracta for discharge and constant head

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Created Area of Mouthpiece in Borda's Mouthpiece Running Free

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Created Area of Mouthpiece in Borda's Mouthpiece Running Full

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Created Area of Orifice given Time of Emptying Hemispherical Tank

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Created Area of Tank given Time for Emptying Tank

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Created Coefficient of Contraction given Area of Orifice

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Created Horizontal distance for coefficient of velocity and vertical distance

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Created Vertical distance for coefficient of velocity and horizontal distance

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Created Area of Nozzle at Outlet for Maximum Power Transmission through Nozzle

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Created Area of Pipe for Maximum Power Transmission through Nozzle

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Created Diameter of Equivalent Pipe

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Created Diameter of nozzle for maximum power transmission through nozzle

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Created Length of Equivalent Pipe

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Created Length of pipe for maximum power transmission through nozzle

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Created Maximum Area of Obstruction in Pipe

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Created Feed Force

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Created Radial Force

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Created Side Cutting Edge Angle for Orthogonal Cutting

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Created Side Rake Angle for Orthogonal Cutting

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6 More Geometry of Turning Process Calculators

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Verified Glide angle for given lift-to-drag ratio

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5 More Gliding Flight Calculators

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Verified Ratio of Stagnation and Static Pressure

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17 More Governing Equations and Sound Wave Calculators

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Verified Load factor for given turn radius for high-performance fighter aircraft

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Verified Turn radius for high load factor

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Verified Turn Rate for given Lift Coefficient

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Verified Velocity for given pull-up maneuver rate

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Verified Velocity given Turn Radius for High Load Factor

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12 More High Load Factor Maneuver Calculators

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Verified Pressure Ratio of Blunt-Nosed Cylinder (First Approximation)

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Verified Radial Coordinate of Blunt-Nosed Cylinder (First Approximation)

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Verified Radius for Cylinder-Wedge Body Shape

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Verified Radius for Sphere-Cone Body Shape

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5 More Hypersonic Flight Paths Velocity of Altitude Map Calculators

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Verified Change in Velocity for Hypersonic Flow in X Direction

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Verified Coefficient of Pressure with Slenderness Ratio and Similarity Constant

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Verified Constant G used for Finding Location of Perturbed Shock

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Verified Density Ratio with Similarity Constant having Slenderness Ratio

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Verified Distance from Tip of Leading Edge to Base

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Verified Non Dimensionalised Time

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11 More Hypersonic Flow and Disturbances Calculators

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Verified Mach Ratio at High Mach Number

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Verified Pressure Ratio for High Mach Number

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Verified Pressure Ratio having High Mach Number with Similarity Constant

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17 More Hypersonic Flow Parameters Calculators

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Verified Dynamic Viscosity around Wall

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Verified Local Shear Stress at Wall

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Verified Static Density Equation using Skin Friction Coefficient

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Verified Static Velocity Equation using Skin Friction Coefficient

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Verified Static Viscosity Relation using Temperature of Wall

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2 More Hypersonic Flow Parameters Calculators

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Verified Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point

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Verified Eddy Viscosity Calculation

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Verified Local Mach Number using Reynolds Number Equation at Transition Region

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Verified Location of Transition Point

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Verified Prandtl Number of Transition Flow

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Verified Specific Heat at Constant Pressure for Transient Flow

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Verified Static Density at Transition Point

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Verified Static Density Equation using Boundary-Layer Momentum Thickness

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Verified Static Velocity at Transition Point

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Verified Static Velocity using Boundary-Layer Momentum Thickness

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Verified Static Viscosity at Transition Point

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Verified Static Viscosity Equation using Boundary-Layer Momentum Thickness

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Verified Transition Reynolds Number

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3 More Hypersonic Transition Calculators

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Created Dimensions of Rankine half-body

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Created Distance of stagnation point S from source in flow past half body

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Created Location of stagnation point on x-axis

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Created Radial velocity at any radius

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Created Radius at any point considering radial velocity

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Created Radius of Rankine circle

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Created Stream function at point

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Created Stream Function at Point in Combined Flow

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Created Stream function in sink flow for angle

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Created Strength of doublet for stream function

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Created Strength of source for radial velocity and at any radius

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Created Strength of source for Rankine half body

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Created Uniform flow velocity for Rankine half body

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Created Uniform flow velocity for stream function at point in combined flow

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9 More Incompressible Flow Characteristics Calculators

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Created Actual Discharge in Venturimeter

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Created Angular Velocity of Vortex using Depth of Parabola

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Created Coefficient of pitot-tube for velocity at any point

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Created Depth of Parabola formed at Free Surface of Water

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Created Difference in Pressure Head for heavier Liquid in Manometer

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Created Difference in pressure head for light liquid in manometer

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Created Height or depth of paraboloid for volume of air

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Created Rate of flow or discharge

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Created Resultant bend force along x and y direction

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Created Resultant velocity for two velocity components

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Created Total Pressure Force at Bottom of Cylinder

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Created Total pressure force on top of cylinder

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Created Velocity at any point for coefficient of pitot-tube

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4 More Kinematics of Flow Calculators

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Verified Freestream Density by Kutta-Joukowski Theorem

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Verified Freestream Velocity by Kutta-Joukowski Theorem

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2 More Kutta Joukowski Lift Theorem Calculators

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Verified Newtonian Dynamic Pressure

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Verified Newtonian Pressure Distribution over Surface using Cosine Angle

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Verified Nusselt Number at Stagnation Point

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Verified Nusselt Number for Stagnation Point on Blunt Body

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Verified Stagnation Pressure

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2 More Laminar Boundary Layer at Stagnation point on Blunt body Calculators

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Verified Touchdown velocity

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4 More Landing Calculators

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Verified Aircraft forward velocity for given normal component of side velocity

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Verified Aircraft sideslip velocity for given dihedral angle

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Verified Dihedral angle for given sideslip velocity

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Verified Normal component of aircraft side velocity for given dihedral angle

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Verified Normal component of aircraft side velocity for given forward velocity

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Created Angle of Attack for Circulation developed on Airfoil

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Created Angle of Attack for Lift Coefficient on Airfoil

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Created Chord Length for Circulation developed on Airfoil

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Created Circulation developed on Airfoil

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Created Circulation for Single Stagnation Point

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Created Circulation in Location of Stagnation Points

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Created Coefficient of Lift for Airfoil

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Created Lift coefficient for lift force in body moving on fluid

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Created Lift Coefficient for Rotating Cylinder with Circulation

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Created Lift Coefficient for Rotating Cylinder with Tangential Speed

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Created Lift Force for body moving in Fluid of Certain Density

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Created Lift Force on Cylinder for Circulation

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Created Radius of Cylinder for Lift Coefficient in Rotating Cylinder with Circulation

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Created Tangential Velocity of Cylinder with Lift Coefficient

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Created Velocity of Airfoil for Circulation developed on Airfoil

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1 More Lift and Circulation Calculators

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Verified Coefficient of Lift for given thrust and weight

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Verified Lift Coefficient given Minimum required Thrust

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Verified Lift-to-Drag Ratio given required Thrust of Aircraft

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Verified Total Drag Force given required Power

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Verified Zero-lift drag coefficient at minimum required thrust

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Verified Zero-Lift Drag Coefficient given required Thrust

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13 More Lift and Drag Requirements Calculators

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Verified 2-D Lift Coefficient for Cylinder

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Verified Stream Function for Lifting Flow over Circular Cylinder

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8 More Lifting Flow over Cylinder Calculators

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Verified Local Heat Transfer Rate Calculation using Stanton Number

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Verified Local Heat Transfer Rate using Nusselt's Number

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Verified Stanton Number for Hypersonic Vehicle

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Verified Static Density Equation using Stanton Number

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Verified Static Velocity using Stanton Number

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Verified Thermal Conductivity at Edge of Boundary Layer Equation using Nusselt's Number

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3 More Local Heat Transfer for Hypersonic Flow Calculators

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Created Absolute Temperature for Velocity of Sound Wave in Isothermal Process

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Created Absolute Temperature for Velocity of Sound Wave using Adiabatic Process

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Created Density of Fluid considering Velocity at Outlet of Orifice

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Created Pressure at Inlet considering Maximum Flow Rate of Fluid

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Created Pressure at Inlet of Tank or Vessel considering Compressible Fluid Flow

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Created Velocity of Sound Wave using Adiabatic Process

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Created Velocity of Sound Wave using Isothermal Process

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Verified Coefficient of Drag Equation with Coefficient of Normal Force

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Verified Exact Normal Shock Wave Maximum Coefficient of Pressure

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Verified Force Exerted on Surface given Static Pressure

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Verified Mass Flux Incident on Surface Area

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Verified Maximum Pressure Coefficient

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9 More Newtonian Flow Calculators

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Verified Tangential Velocity for Non-Lifting Flow over Circular Cylinder

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9 More Nonlifting Flow over Cylinder Calculators

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Verified Component of Downstream Mach Number Normal to Oblique Shock for given Normal Upstream Mach Number

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Verified Density behind Oblique Shock for given Upstream Density and Normal Upstream Mach Number

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Verified Density Ratio across Oblique Shock

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Verified Pressure behind Oblique Shock for given Upstream Pressure and Normal Upstream Mach Number

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Verified Pressure Ratio across Oblique Shock

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Verified Temperature behind Oblique Shock for given Upstream Temperature and Normal Upstream Mach Number

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Verified Temperature Ratio across Oblique Shock

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3 More Oblique Shock Calculators

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Verified Parallel Upstream Flow Components after Shock as Mach Tends to Infinite

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Verified Perpendicular Upstream Flow Components behind Shock Wave

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13 More Oblique Shock Relation Calculators

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Verified Friction Coefficient

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20 More Others and Extra Calculators

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Verified Energy for Blast Wave

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Verified Radial Coordinate of Blunt Slab Blast Wave

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Verified Time Required for Blast Wave

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5 More Planar and Blunt Slab Blast Wave Calculators

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Created Efficiency of power transmission in flow through pipes

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Created Efficiency of Power Transmission through Nozzle

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Created Efficiency of power transmission through nozzle for velocity and total head

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Created Power Lost ue to Sudden Enlargement

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Created Power transmission through pipes

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Verified Power required at Altitude

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Verified Power required at Altitude given Power at sea-level

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15 More Preliminary Aerodynamics Calculators

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Created Difference in liquid level in three compound pipes with same friction coefficient

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Created Head available at Base of Nozzle

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Created Head Loss due to Friction for Efficiency of Power Transmission

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Created Intensity of pressure wave produced for gradual closure of valves

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Created Loss of Head at Entrance of Pipe

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Created Loss of head at exit of pipe

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Created Loss of Head due to Bend in Pipe

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Created Loss of Head due to Obstruction in Pipe

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Created Loss of Head due to Sudden Contraction

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Created Loss of head due to sudden enlargement at any particular section of pipe

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Created Loss of head in equivalent pipe

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Created Total head at inlet of pipe for head available at base of nozzle

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Created Total head available at inlet of pipe for efficiency of power transmission

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1 More Pressure and Flow Head Calculators

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Verified Endurance of Propeller-Driven Airplane

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Verified Power Available for Reciprocating Engine-Propeller Combination

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Verified Propeller Efficiency for given Endurance of Propeller-Driven Airplane

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Verified Propeller Efficiency for given Range and Lift-to-Drag Ratio of Propeller-Driven Airplane

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Verified Propeller Efficiency for given Range of Propeller-Driven Airplane

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Verified Propeller Efficiency for Reciprocating Engine-Propeller Combination

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Verified Range of Propeller-Driven Airplane

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Verified Range of Propeller-Driven Airplane for given lift-to-drag ratio

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Verified Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane

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Verified Specific Fuel Consumption for given Range and Lift-to-Drag Ratio of Propeller-Driven Airplane

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Verified Specific Fuel Consumption for given Range of Propeller-Driven Airplane

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11 More Propeller Driven Airplane Calculators

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Verified Static Enthalpy Ratio across Normal Shock

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Verified Temperature Ratio across Normal Shock

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4 More Property Change Across Shock Waves Calculators

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Verified Load Factor given Pull-Down Maneuver Radius

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Verified Load Factor given Pull-Up Maneuver Rate

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Verified Pull-down maneuver radius

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Verified Pull-Up Maneuver Rate

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Verified Velocity for given Pull-Down Maneuver Rate

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Verified Velocity for given Pull-Up Maneuver Radius

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6 More Pull Up and Pull Down Maneuver Calculators

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Verified Chord Length for Flat Plate Case

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Verified Local Reynolds Number

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Verified Mach Number at Reference Temperature

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Verified Overall Skin-Friction Drag Coefficient for Incompressible Flow

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Verified Reference Temperature Equation

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Verified Stanton Number Obtained from Classical Theory

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Verified Static Viscosity of Plate using Chord Length for Flat Plate Case

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Verified Wall Temperature using Reference Temperature

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7 More Reference Temperature Method Calculators

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Verified Detachment Distance of Cylinder Wedge Body Shape

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Verified Detachment Distance of Sphere Cone Body Shape

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Verified Grid Point Calculation for Shock Waves

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Verified Nose Radius of Cylinder-Wedge

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Verified Nose Radius of Sphere Cone

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Verified Pressure Ratio for Unsteady Waves

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Verified Ratio of New and Old Temperature

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3 More Shock Dynamics and Aerodynamic Shape Calculators

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Verified Inner Surface Temperature of Plane Wall

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Verified Temperature at Distance x from Inner Surface in Wall

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Verified Thermal Resistance of Wall

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5 More Single Plane Wall Calculators

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Verified Radial Velocity for 2-D Incompressible Source Flow

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Verified Stream Function for Semi-Infinite Body

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5 More Source Flow Calculators

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Verified Coefficient of Pressure Equation using Specific Heat Ratio

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Verified Curvilinear Grid Location Equation

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Verified Density Equation using Enthalpy and Pressure

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Verified Enthalpy Equation using Pressure and Density

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Verified Pressure Equation using Enthalpy and Density

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6 More Space Marching Finite Difference Method Additional Solutions of the Euler Equations Calculators

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Created Density of Fluid for Stagnation considering Compressible Fluid Flow

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Created Stagnation Density considering other Stagnation Properties of Fluid

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Created Stagnation Density given Compressible Fluid Flow

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Created Stagnation Pressure considering other Stagnation Properties of Fluid

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Created Stagnation Pressure for Compressible Fluid Flow

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Created Stagnation Temperature considering Compressible Fluid Flow

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Created Stagnation Temperature considering other Stagnation Properties of Fluid

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Created Temperature of Fluid for Stagnation Temperature considering Compressible Fluid Flow

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Verified Static Density of Fluid over Flat Plate

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Verified Static Temperature over Flat Plate using Static Mach Number

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Verified Static Viscosity using Wall Temperature and Static Temperature

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3 More Static Parameters for Hypersonic Flow Calculators

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Verified Elevator Area given Hinge Moment Coefficient

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Verified Elevator Area given Stick Force

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Verified Elevator Hinge moment coefficient

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Verified Elevator Hinge Moment given Hinge Moment Coefficient

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Verified Flight Velocity for given Stick Force

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Verified Gearing Ratio

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Verified Gearing Ratio given Hinge Moment Coefficient

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Verified Hinge Moment for given Gearing Ratio

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Verified Hinge Moment for given Stick Force

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Verified Stick Deflection Angle for given Stick Force

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Verified Stick Length for given Stick Force

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12 More Stick Forces and Hinge Moments Calculators

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Verified Large Mach Number over Flat Plate using Static Temperature and Wall Temperature

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Verified Pressure Ratio for Cold-Wall Case Strong Interaction

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Verified Pressure Ratio for Cold-Wall Case Weak Interaction

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Verified Viscosity of Wall using Wall Temperature and Static Temperature

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Verified Wall Density of Fluid over Flat Plate

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3 More Supersonic Aerothermodynamics Calculators

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Verified Tail Area for given Tail Moment Coefficient

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Verified Tail Efficiency for given Pitching Moment Coefficient

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Verified Tail Lift for given Tail Pitching Moment

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Verified Tail Moment Arm for given Tail Moment Coefficient

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Verified Tail Pitching Moment Coefficient

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Verified Tail Pitching Moment Coefficient for given Tail Efficiency

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Verified Tail Pitching Moment for given Lift Coefficient

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12 More Tail Contribution Calculators

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Verified Liftoff velocity for given weight

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14 More Take Off Calculators

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Verified Mach Number

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Verified Stagnation Temperature

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17 More Thermodynamics and Governing Equations Calculators

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Verified Minimum Thrust required for given Lift Coefficient

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Verified Power required for given total drag force

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Verified Thrust for given coefficients of lift and drag

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Verified Thrust of aircraft required for given Lift-to-drag ratio

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Verified Weight of Aircraft for given Coefficients of Lift and Drag

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Verified Weight of Aircraft for given Lift-to-Drag Ratio

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13 More Thrust and Power Requirements Calculators

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Created Thrust force for given cutting force, shear angle and force along shear force

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Created Thrust force for given cutting force, shear angle and force normal to shear force

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2 More Thrust Force Calculators

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Created Average Height of Irregularities for Turbulent Flow in Pipes

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Created Discharge through Pipe given Head Loss in Turbulent Flow

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Created Head Loss due to Friction given Power Required in Turbulent Flow

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Created Power Required to Maintain Turbulent Flow

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Created Roughness Reynold Number for Turbulent Flow in Pipes

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Created Shear Stress Developed for Turbulent Flow in Pipes

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Created Shear Velocity for Turbulent Flow in Pipes

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11 More Turbulent Flow Calculators

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Verified Stream Function for Uniform Incompressible Flow

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3 More Uniform Flow Calculators

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Created Coefficient of velocity

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Created Coefficient of velocity for horizontal and vertical distance

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Created Coefficient of Velocity given Head Loss

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Created Theoretical velocity

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Created Time of Emptying Circular Horizontal Tank

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Created Time of Emptying Hemispherical Tank

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Created Time of Emptying Tank through Orifice at Bottom

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Created Velocity of liquid at C-C for Hc, Ha, and H

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Verified Aerodynamic Heating Equation for Stanton number

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Verified Coefficient of Friction using Stanton Number for Flat Plate Case

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Verified Drag per Unit Span

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Verified Prandtl Number for Flat Plate with Viscous Flow

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Verified Recovery Factor using Temperature

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Verified Skin-Friction Drag for Flat Plate in Viscous Flow

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Verified Static Density Equation using Aerodynamic Equation

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Verified Static Velocity Equation using Aerodynamic Heating Equation

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7 More Viscous Flow Calculators

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Verified Stream Function for 2-D Vortex Flow

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2 More Vortex Flow Calculators

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Verified Wall Temperature over Flat Plate using Static Mach Number

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3 More Wall Temperature Calculators

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Verified Angle of incidence of tail

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Verified Lift due to Tail only

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Verified Lift due to Wing only

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Verified Tail area for given tail efficiency

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Verified Tail Efficiency for given lift coefficients

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Verified Tail Lift Coefficient for given Pitching Moment

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Verified Tail Lift Coefficient for given Pitching Moment Coefficient

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Verified Tail Lift Coefficient of Wing-Tail Combination

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Verified Total Lift of Wing-Tail Combination

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Verified Wing Lift Coefficient of wing-tail combination

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5 More Wing Tail Contribution Calculators

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Verified Wing Area for given Moment Produced by Vertical Tail

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Verified Wing Dynamic Pressure for given Yawing Moment Coefficient

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Verified Wingspan for given Yawing Moment Coefficient

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9 More Wing Tail Interaction Calculators

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List of Calculators by Maiarutselvan V