Calculator A to Z

Calculators Created by Shikha Maurya

Shikha Maurya
Indian Institute of Technology (IIT), Bombay
https://www.linkedin.com/in/shikha-maurya-eager-to-learn/
108
Formulas Created
170
Formulas Verified
75
Across Categories

List of Calculators by Shikha Maurya

Following is a combined list of all the calculators that have been created and verified by Shikha Maurya. Shikha Maurya has created 108 and verified 170 calculators across 75 different categories till date.
Aero Thermal Dynamics (3)
Verified Non Dimensional Internal Energy Parameter using Wall-to-Freestream Temperature Ratio
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Verified Non Dimensional Static Enthalpy
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Verified Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow
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13 More Aero Thermal Dynamics Calculators
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Aerodynamic Measurements and Wind Tunnel Testing (10)
Created Airspeed Measurement by Pitot Tube
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Created Airspeed Measurement by Venturi
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Created Dynamic Pressure in Incompressible Flow
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Created Height Difference of Manometric Fluid for given Pressure Difference
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Created Surface Pressure on Body using Pressure Coefficient
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Created Test Section Velocity by Manometric Height for Wind Tunnel
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Created Total Pressure in Incompressible Flow
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Created Wind Tunnel Pressure Difference by Manometer
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Created Wind Tunnel Pressure Difference with Test Speed
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Created Wind Tunnel Test Section Velocity
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Aerodynamic Parameters (1)
Verified Yawing Moment Coefficient using Wingspan
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10 More Aerodynamic Parameters Calculators
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Aircraft Dynamics Nomenclature (8)
Verified Aerodynamic Axial Force
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Verified Aerodynamic Normal Force
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Verified Aerodynamic Side Force
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Verified Angle of attack
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Verified Pitching moment
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Verified Pitching moment coefficient
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Verified Side force coefficient
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Verified Sideslip angle
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10 More Aircraft Dynamics Nomenclature Calculators
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Atmosphere and Gas Properties (5)
Verified Absolute altitude
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Verified Geometric altitude
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Verified Geometric altitude for given geopotential altitude
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Verified Geopotential altitude
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Verified Lapse rate
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9 More Atmosphere and Gas Properties Calculators
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Bending Stresses (1)
Verified Section Modulus of Steel Beam given Stress in Steel for Unshored Members
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9 More Bending Stresses Calculators
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Bernoulli's Equation and Pressure Concepts (6)
Created Pressure at Downstream Point by Bernoulli's Equation
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Created Pressure at Upstream Point by Bernoulli's Equation
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Created Pressure Coefficient
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Created Pressure Coefficient using Velocity Ratio
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Created Static Pressure in Incompressible Flow
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Created Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity
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Blast Wave Part Theory (3)
Verified Pressure Coefficient Combined with Blast Wave for Shuttle
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Verified Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack
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Verified Pressure Coefficient for Blunt-Nosed Cylinder
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3 More Blast Wave Part Theory Calculators
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Body Lying on Rough Horizontal Plane (1)
Verified Acceleration of System with Bodies One Hanging Free and Other Lying on Rough Horizontal Plane
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1 More Body Lying on Rough Horizontal Plane Calculators
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Body Lying on Smooth Horizontal Plane (2)
Verified Acceleration in System
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Verified Tension in String if only One Body is Freely Suspended
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Body Passing Over Smooth Pulley (3)
Verified Acceleration of Bodies
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Verified Mass of Body B of Smaller Mass
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Verified Tension in String if Both Bodies are Freely Hanging
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Boundary Layer Flow (4)
Verified Drag Force on Plate
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Verified Reynold Number for Drag Force on Plate
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Verified Viscosity of Liquid for Drag Force on Plate
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Verified Width of Plate for Drag Force on Plate
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17 More Boundary Layer Flow Calculators
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Climbing Flight (2)
Verified Excess power
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Verified Total Drag for given Excess Power
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14 More Climbing Flight Calculators
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Compressible Flow Parameters (3)
Verified Mach Angle for Compressible Fluid Flow
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Verified Velocity of Projectile of Mach Cone in Compressible Fluid Flow
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Verified Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow
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7 More Compressible Flow Parameters Calculators
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Compression Waves (2)
Verified Density before Shock Formation for Compression Wave
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Verified Temperature Ratio for Unsteady Compression Waves
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1 More Compression Waves Calculators
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Cutting Force (3)
Created Cutting force for given force along shear force, shear, friction and normal rake angles
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Created Cutting force for given resultant force in merchant circle, friction angle and normal rake angle
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Created Cutting force for shear stress, width of cut, uncut chip thickness, friction, rake and shear angles
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3 More Cutting Force Calculators
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Cylindrical Blast Wave (2)
Verified Modified Pressure Equation for Cylindrical Blast Wave
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Verified Pressure Ratio for Blunt Slab Blast Wave
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6 More Cylindrical Blast Wave Calculators
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Dimensionless Quantities (1)
Verified Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number
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3 More Dimensionless Quantities Calculators
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Dimensions and Geometry (4)
Verified Length for Difference of Pressure in Viscous Flow between Two Parallel Plates
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Verified Length for Pressure Head Loss in Viscous Flow between Two Parallel Plates
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Verified Length of Tube in Capillary Tube Method
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Verified Radius of Capillary Tube
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15 More Dimensions and Geometry Calculators
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Discharge (4)
Verified Discharge over Rectangle Weir Considering Bazin's formula
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Verified Discharge over Rectangle Weir Considering Francis's formula
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Verified Discharge with Velocity of Approach
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Verified Discharge without Velocity of Approach
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13 More Discharge Calculators
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Doublet Flow (2)
Created Stream Function for 2-D Doublet Flow
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Created Velocity Potential for 2-D Doublet Flow
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Downstream Shock Waves (10)
Created Density behind Normal Shock given Upstream Density and Mach Number
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Created Density behind Normal Shock using Normal Shock Momentum Equation
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Created Enthalpy behind Normal Shock from Normal Shock Energy Equation
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Created Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula
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Created Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number
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Created Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number
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Created Static Pressure behind Normal Shock using Normal Shock Momentum Equation
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Created Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number
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Created Velocity behind Normal Shock by Normal Shock Momentum Equation
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Created Velocity behind Normal Shock from Normal Shock Energy Equation
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5 More Downstream Shock Waves Calculators
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Drag and Forces (3)
Verified Area of body for Lift Force in body moving on Fluid
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Verified Pressure Drag from Total Drag Force on Sphere
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Verified Skin Friction Drag from Total Drag Force on Sphere
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8 More Drag and Forces Calculators
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Expansion Waves (2)
Verified New Pressure after Shock Formation, Subtracted to Velocity for Expansion Wave
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Verified Pressure Ratio for Unsteady Waves with Subtracted Induced Mass Motion for Expansion Waves
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3 More Expansion Waves Calculators
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Expansion Waves (9)
Created Flow Deflection Angle using Prandtl Meyer Function
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Created Forward Mach Angle of Expansion Fan
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Created Prandtl Meyer Function
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Created Prandtl Meyer Function at Upstream Mach Number
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Created Pressure behind Expansion Fan
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Created Pressure Ratio across Expansion Fan
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Created Rearward Mach Angle of Expansion Fan
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Created Temperature behind Expansion Fan
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Created Temperature Ratio across Expansion Fan
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1 More Expansion Waves Calculators
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Flow Analysis (4)
Verified Difference of Pressure for Viscous Flow between Two Parallel Plates
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Verified Loss of Pressure Head for Viscous Flow between Two Parallel Plates
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Verified Power Absorbed in Overcoming Viscous Resistance in Journal Bearing
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Verified Viscosity of Fluid or Oil for Capillary Tube Method
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9 More Flow Analysis Calculators
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Flow over Airfoils (8)
Created Boundary Layer Thickness for Laminar Flow
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Created Boundary Layer Thickness for Turbulent Flow
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Created Center of Pressure Location for Cambered Airfoil
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Created Lift Coefficient for Cambered Airfoil
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Created Lift Coefficient for Symmetrical Airfoil by Thin Airfoil Theory
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Created Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory
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Created Skin Friction Drag Coefficient for Flat Plate in Laminar Flow
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Created Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow
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Flow Regime (4)
Verified Discharge in Equivalent Pipe
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Verified Velocity of Flow at Outlet of Nozzle
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Verified Velocity of Flow at outlet of Nozzle for Efficiency and Head
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Verified Velocity of fluid in pipe for head loss at entrance of pipe
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13 More Flow Regime Calculators
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Fluid Flow and Resistance (6)
Verified Discharge in Capillary Tube Method
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Verified Rotational Speed considering Power Absorbed and Torque in Journal Bearing
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Verified Shear Force for Torque and Diameter of Shaft in Journal Bearing
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Verified Shear Stress in Fluid or Oil of Journal Bearing
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Verified Torque Required Considering Power Absorbed in Journal Bearing
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Verified Torque Required to Overcome Shear Force in Journal Bearing
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15 More Fluid Flow and Resistance Calculators
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Force Along Shear (1)
Created Force along shear force for given R of merchant circle, shear, friction, and normal rake angles
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2 More Force Along Shear Calculators
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Force Normal to Shear (1)
Created Shear angle for given Resultant force, force along shear force, friction, and normal rake angles
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3 More Force Normal to Shear Calculators
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Forces and Friction (1)
Created Friction angle for given R of merchant circle, force along shear, shear, and normal rake angle
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5 More Forces and Friction Calculators
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Geometric DImension (4)
Verified Length of Weir Considering Bazin's formula without Velocity of Approach
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Verified Length of Weir Considering Francis's formula
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Verified Length of Weir or Notch for Velocity of Approach
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Verified Length of Weir or Notch without Velocity of Approach
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6 More Geometric DImension Calculators
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Geometric Property (6)
Verified Area of Nozzle at Outlet for Maximum Power Transmission through Nozzle
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Verified Area of Pipe for Maximum Power Transmission through Nozzle
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Verified Diameter of Equivalent Pipe
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Verified Diameter of nozzle for maximum power transmission through nozzle
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Verified Length of Equivalent Pipe
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Verified Length of pipe for maximum power transmission through nozzle
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1 More Geometric Property Calculators
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Geometry and Dimensions (2)
Created Uncut chip thickness given cutting force, shear stress, cut, friction, normal rake and shear angles
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Created Width of cut given cutting force, shear stress, uncut chip, friction, normal rake and shear angles
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6 More Geometry and Dimensions Calculators
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Governing Equations and Sound Wave (4)
Created Critical Density
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Created Critical Pressure
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Created Critical Temperature
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Created Isentropic Compressibility for given Density and Speed of Sound
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14 More Governing Equations and Sound Wave Calculators
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High Load Factor Maneuver (5)
Verified Lift Coefficient for given Turn Rate
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Verified Load factor for given turn rate for high-performance fighter aircraft
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Verified Radius of Turn for given Lift Coefficient
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Verified Radius of Turn for given Wing Loading
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Verified Turn Rate for given Wing Loading
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12 More High Load Factor Maneuver Calculators
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Hypersonic Flight Paths Velocity of Altitude Map (1)
Verified Blunt-Nosed Radial Coordinate Flat Plate (First Approximation)
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8 More Hypersonic Flight Paths Velocity of Altitude Map Calculators
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Hypersonic Flow Parameters (1)
Verified Skin Friction Coefficient for Incompressible Flow
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6 More Hypersonic Flow Parameters Calculators
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Incompressible Flow Characteristics (1)
Verified Distance of stagnation point S from source in flow past half body
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22 More Incompressible Flow Characteristics Calculators
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Kinematics of Flow (2)
Verified Coefficient of pitot-tube for velocity at any point
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Verified Resultant bend force along x and y direction
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15 More Kinematics of Flow Calculators
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Kutta Joukowski Lift Theorem (4)
Created Circulation by Kutta-Joukowski Theorem
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Created Freestream Density by Kutta-Joukowski Theorem
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Created Freestream Velocity by Kutta-Joukowski Theorem
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Created Lift Per Unit Span by Kutta-Joukowski Theorem
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Landing (1)
Verified Stall velocity for given touchdown velocity
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4 More Landing Calculators
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Lift and Circulation (6)
Verified Angle of Attack for Circulation developed on Airfoil
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Verified Chord Length for Circulation developed on Airfoil
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Verified Circulation developed on Airfoil
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Verified Lift coefficient for lift force in body moving on fluid
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Verified Lift Force for body moving in Fluid of Certain Density
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Verified Velocity of Airfoil for Circulation developed on Airfoil
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10 More Lift and Circulation Calculators
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Lifting Flow over Cylinder (6)
Created 2-D Lift Coefficient for Cylinder
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Created Location of Stagnation Point Outside Cylinder for Lifting Flow
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Created Radial Velocity for Lifting Flow over Circular Cylinder
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Created Stream Function for Lifting Flow over Circular Cylinder
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Created Surface Pressure Coefficient for Lifting Flow over Circular Cylinder
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Created Tangential Velocity for Lifting Flow over Circular Cylinder
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4 More Lifting Flow over Cylinder Calculators
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Local Heat Transfer for Hypersonic Flow (3)
Verified Adiabatic Wall Enthalpy using Stanton Number
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Verified Enthalpy of Wall using Stanton Number
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Verified Nusselt Number for Hypersonic Vehicle
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6 More Local Heat Transfer for Hypersonic Flow Calculators
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Nonlifting Flow over Cylinder (5)
Created Radial Velocity for Non-Lifting Flow over Circular Cylinder
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Created Radius of Cylinder for Non-Lifting Flow
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Created Stream Function for Non-Lifting Flow over Circular Cylinder
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Created Surface Pressure Coefficient for Non-Lifting Flow over Circular Cylinder
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Created Tangential Velocity for Non-Lifting Flow over Circular Cylinder
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5 More Nonlifting Flow over Cylinder Calculators
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Normal Shock Relations (2)
Created Critical Speed of Sound from Prandtl Relation
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Created Upstream Velocity using Prandtl Relation
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5 More Normal Shock Relations Calculators
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Number of Connectors in Bridges (5)
Verified Effective Concrete Area given Force in Slab
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Verified Force in Slab at Maximum Positive Moments given Minimum Number of Connectors for Bridges
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Verified Force in Slab given Effective Concrete Area
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Verified Minimum Number of Connectors for Bridges
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Verified Steel Yield Strength given Total Area of Steel Section
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13 More Number of Connectors in Bridges Calculators
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Oblique Shock (7)
Created Component of Downstream Mach Number Normal to Oblique Shock for given Normal Upstream Mach Number
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Created Density behind Oblique Shock for given Upstream Density and Normal Upstream Mach Number
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Created Density Ratio across Oblique Shock
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Created Pressure behind Oblique Shock for given Upstream Pressure and Normal Upstream Mach Number
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Created Pressure Ratio across Oblique Shock
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Created Temperature behind Oblique Shock for given Upstream Temperature and Normal Upstream Mach Number
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Created Temperature Ratio across Oblique Shock
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3 More Oblique Shock Calculators
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Planar and Blunt Slab Blast Wave (1)
Verified Pressure Ratio for Blunt Cylinder Blast Wave
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7 More Planar and Blunt Slab Blast Wave Calculators
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Power Transmission (2)
Verified Efficiency of Power Transmission through Nozzle
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Verified Efficiency of power transmission through nozzle for velocity and total head
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3 More Power Transmission Calculators
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Preliminary Aerodynamics (3)
Verified Power required at sea-level conditions
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Verified Velocity at Altitude given Velocity at Sea-Level
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Verified Velocity at Sea-Level given Lift Coefficient
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14 More Preliminary Aerodynamics Calculators
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Pressure and Flow Head (2)
Verified Loss of Head at Entrance of Pipe
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Verified Loss of head in equivalent pipe
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12 More Pressure and Flow Head Calculators
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Property Change Across Shock Waves (4)
Created Density Ratio across Normal Shock
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Created Pressure Ratio across Normal Shock
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Created Static Enthalpy Ratio across Normal Shock
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Created Temperature Ratio across Normal Shock
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2 More Property Change Across Shock Waves Calculators
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Pull Up and Pull Down Maneuver (1)
Verified Velocity given Pull-down Maneuver Radius
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11 More Pull Up and Pull Down Maneuver Calculators
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Reference Temperature Method (1)
Verified Overall Skin-Friction Drag Coefficient
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14 More Reference Temperature Method Calculators
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Resultants and Stress (4)
Created Normal rake angle for given Resultant force, force along shear, shear, and friction angle
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Created R in merchant circle for given force along shear force, shear, friction and normal rake angles
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Created Resultant force in merchant circle for given cutting force, friction and normal rake angles
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Created Shear stress given cutting force, cut size, uncut chip thickness, friction, rake and shear angles
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2 More Resultants and Stress Calculators
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Shear Range (1)
Verified Horizontal Shear Range at Juncture of Slab and Beam
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11 More Shear Range Calculators
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Shock Dynamics and Aerodynamic Shape (3)
Verified Local Shock Velocity Equation
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Verified Mach Wave behind Shock
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Verified Mach Wave behind Shock with Mach Infinity
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7 More Shock Dynamics and Aerodynamic Shape Calculators
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Source Flow (7)
Created Radial Velocity for 2-D Incompressible Source Flow
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Created Source Strength for 2-D Incompressible Source Flow
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Created Stagnation Streamline Equation for Flow over Semi-Infinite Body
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Created Stream Function for 2-D Incompressible Source Flow
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Created Stream Function for Flow over Rankine Oval
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Created Stream Function for Semi-Infinite Body
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Created Velocity Potential for 2-D Source Flow
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Space Marching Finite Difference Method Additional Solutions of the Euler Equations (3)
Verified Enthalpy Equation using Coefficient of Pressure for Calorically Perfect Gas
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Verified Free Stream Enthalpy
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Verified Total Specific Enthalpy
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8 More Space Marching Finite Difference Method Additional Solutions of the Euler Equations Calculators
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Stick Forces and Hinge Moments (6)
Verified Elevator Chord Length given Hinge Moment Coefficient
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Verified Elevator Deflection Angle for given Stick Force
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Verified Elevator Stick Force
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Verified Elevator Stick Force given Hinge Moment Coefficient
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Verified Gearing Ratio for given Stick Force
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Verified Stick Deflection Angle for given Gearing Ratio
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17 More Stick Forces and Hinge Moments Calculators
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Tail Contribution (7)
Verified Horizontal tail area for given tail volume ratio
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Verified Horizontal tail volume ratio
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Verified Pitching Moment due to Tail
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Verified Tail moment arm for given horizontal tail volume ratio
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Verified Tail Pitching Moment for given Moment Coefficient
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Verified Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio
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Verified Wing Reference Area for given Horizontal Tail Volume Ratio
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12 More Tail Contribution Calculators
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Take Off (10)
Verified Coefficient of rolling friction during ground roll
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Verified Drag during ground effect
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Verified Ground effect factor
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Verified Lift acting on aircraft during ground roll
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Verified Liftoff distance
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Verified Maximum Lift coefficient for given liftoff velocity
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Verified Resistance force during ground roll
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Verified Stall velocity for given weight
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Verified Thrust for given liftoff distance
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Verified Weight of aircraft during ground roll
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5 More Take Off Calculators
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Turbulent Flow (3)
Verified Average Height of Irregularities for Turbulent Flow in Pipes
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Verified Power Required to Maintain Turbulent Flow
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Verified Roughness Reynold Number for Turbulent Flow in Pipes
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15 More Turbulent Flow Calculators
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Turning Flight (7)
Verified Bank angle during level turn
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Verified Load factor given Lift Force and Weight of Aircraft
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Verified Load Factor given Turn Radius
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Verified Turn rate
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Verified Velocity for given turn radius
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Verified Velocity for given turn rate
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Verified Weight for given Load Factor
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6 More Turning Flight Calculators
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Ultimate Shear Strength of Connectors in Bridges (3)
Verified Channel Web Thickness given Ultimate Shear Connector Strength for Channels
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Verified Elastic Modulus of Concrete given Ultimate Shear Connector Strength for Welded Studs
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Verified Ultimate Shear Strength for Welded Studs
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6 More Ultimate Shear Strength of Connectors in Bridges Calculators
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Uniform Flow (4)
Created Stream Function for Uniform Incompressible Flow
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Created Stream Function for Uniform Incompressible Flow in Polar Coordinates
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Created Velocity Potential for Uniform Incompressible Flow
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Created Velocity Potential for Uniform Incompressible Flow in Polar Coordinates
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Upstream Shock Waves (5)
Created Density ahead of Normal Shock using Normal Shock Momentum Equation
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Created Enthalpy ahead of Normal Shock from Normal Shock Energy Equation
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Created Static Pressure ahead of Normal Shock using Normal Shock Momentum Equation
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Created Velocity ahead of Normal Shock by Normal Shock Momentum Equation
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Created Velocity ahead of Normal Shock from Normal Shock Energy Equation
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2 More Upstream Shock Waves Calculators
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Vertical Tail Contribution (8)
Verified Moment Produced by Vertical Tail for given Moment Coefficient
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Verified Moment Produced by Vertical Tail for given Side Force
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Verified Vertical Tail Angle of Attack
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Verified Vertical tail area for given vertical tail volume ratio
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Verified Vertical Tail Moment Arm for given Side Force
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Verified Vertical Tail Moment Arm for given Vertical Tail Volume Ratio
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Verified Vertical Tail Side Force for Given Moment
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Verified Vertical tail volume ratio
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16 More Vertical Tail Contribution Calculators
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Viscous Flow (1)
Verified Total Enthalpy in Inviscid Flow Outside Boundary Layer
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14 More Viscous Flow Calculators
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Vortex Flow (3)
Created Stream Function for 2-D Vortex Flow
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Created Tangential Velocity for 2-D Vortex Flow
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Created Velocity Potential for 2-D Vortex Flow
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Wing Tail Contribution (3)
Verified Angle of Attack at Tail
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Verified Downwash angle
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Verified Total Lift Coefficient of Wing-Tail Combination
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12 More Wing Tail Contribution Calculators
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Wing Tail Interaction (2)
Verified Wing Area for given Vertical Tail Volume Ratio
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Verified Wingspan for given Vertical Tail Volume Ratio
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10 More Wing Tail Interaction Calculators
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Percentage calculator Fraction calculator LCM HCF Calculator
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