Calculators Created by Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
https://www.linkedin.com/in/arendra-sai-venkata-phanindra-chary-1a5b76139
120
Formulas Created
251
Formulas Verified
90
Across Categories

List of Calculators by Sai Venkata Phanindra Chary Arendra

Following is a combined list of all the calculators that have been created and verified by Sai Venkata Phanindra Chary Arendra. Sai Venkata Phanindra Chary Arendra has created 120 and verified 251 calculators across 90 different categories till date.
Verified Charging Current in Relaxation Circuit
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Verified Power Supply during Charging
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Verified Resistance of Charging Circuit
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Verified Time Constant from Charging Current
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Verified Time Elapsed during Charging
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Created Area of Composite Wall of 2 Layers
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Created Heat Flow Rate through Composite Wall of 2 Layers in Series
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Created Inner Surface Temperature of Composite Wall for 2 Layers in Series
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Created Interface Temperature of Composite Wall of 2 Layers given Inner Surface Temperature
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Created Interface Temperature of Composite Wall of 2 Layers given Outer Surface Temperature
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Created Length of 2nd Layer of Composite Wall in Conduction through Walls
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Created Outer Surface Temperature of Composite Wall of 2 Layers for Conduction
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Created Thermal Resistance of Composite Wall with 2 Layers in Series
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Created Area of Composite Wall of 3 Layers
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Created Heat Flow Rate through Composite Wall of 3 Layers in Series
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Created Inner Surface Temperature of Composite Wall of 3 Layers in Series
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Created Length of 3rd Layer of Composite Wall in Conduction through Walls
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Created Outer Surface Temperature of Composite Wall of 3 Layers for Conduction
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Created Thermal Resistance of Composite Wall with 3 Layers in Series
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Created Absorbed Radiation using Absorptivity and Incident Radiation
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Created Absorbed Radiation using Incident, Reflected and Transmitted Radiation
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Created Absorptivity
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Created Absorptivity using Reflectivity and Transmissivity
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Created Absorptivity using Reflectivity for Opaque Surface
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Created Incident Radiation given Reflectivity and Reflected Radiation
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Created Incident Radiation using Absorbed, Reflected and Transmitted Radiation
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Created Incident Radiation using Absorptivity and Absorbed Energy
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Created Incident Radiation using Transmissivity and Transmitted Radiation
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Created Reflected Radiation given Incident, Absorbed and Transmitted Radiation
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Created Reflected Radiation given Reflectivity and Incident Radiation
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Created Reflectivity given Absorptivity and Transmissivity
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Created Reflectivity using Absorptivity for Opaque Surface
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Created Reflectivity using Reflected Radiation and Incident Radiation
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Created Transmissivity given Transmitted Radiation and Incident Radiation
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Created Transmissivity using Absorptivity and Reflectivity
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Created Transmitted Radiation using Incident, Absorbed and Reflected Radiation
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Created Transmitted Radiation using Transmissivity and Incident Radiation
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Verified Diameter of measuring wires ACME threads
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Verified Micrometer measurement per reading acme threads
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Verified Pitch diameter acme threads
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Verified Pitch of screw acme threads
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Verified Internal Energy for Hypersonic Flow
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Verified Non Dimensional Internal Energy Parameter
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Verified Static Enthalpy
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Verified Wall Temperature Calculation using Internal Energy Change
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12 More Aero Thermal Dynamics Calculators
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Verified Non-Dimensional Radius for Hypersonic Vehicles
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Verified Transformed Conical Variable
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9 More Approximate Methods of Hypersonic Inviscid Flowfields Calculators
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Verified Free Stream Enthalpy over Flat Plate with Freestream Conditions
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Verified Free Stream Velocity over Flat Plate using Drag Force
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Verified Free Stream Velocity over Flat Plate with Freestream Conditions
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Verified Freestream Density over Flat under Freestream Flow Conditions
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Verified Pressure Ratio for Insulated Flat Plate, Strong Interaction
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Verified Total Enthalpy over Flat Plate with Freestream Conditions
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9 More Approximate Results Applied to Hypersonic Vehicles Calculators
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Created Diffuse solar radiation given total solar energy and direct radiation
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Created Effective surface temperature of sun given solar constant
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Created Mean distance between sun or star and earth or planet
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Created Radius of sun given total solar irradiance
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Created Total solar energy incident on unit area of horizontal surface on ground
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Created Total solar irradiance or solar constant
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Verified Diameter of Measuring Wires British Threads
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Verified Micrometer Measurement per Reading British Threads
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Verified Pitch diameter British thread
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Verified Pitch of Screw British
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Verified Time Period of Oscillation of Ship
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Verified Volume of body in fluid for metacentric height and BG
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9 More Buoyancy Calculators
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Verified Tolerance Unit
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6 More Clearance fits Calculators
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Verified Centrifugal Force in Accelerated Flight
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Verified Drag in Accelerated Flight
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Verified Excess power for given rate of climb
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Verified Lift in Accelerated Flight
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Verified Thrust in Accelerated Flight
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Verified Velocity in Accelerated Flight
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Verified Velocity of aircraft at given rate of climb
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Verified Velocity of Aircraft for given Excess Power
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8 More Climbing Flight Calculators
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Verified Mach Number for Compressible Fluid Flow
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Verified Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid
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Verified Velocity of Sound Wave given Mach Number for Compressible Fluid Flow
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7 More Compressible Flow Parameters Calculators
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Verified New Pressure after Shock Formation for Compression Wave
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2 More Compression Waves Calculators
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Verified Freestream Density
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Verified Freestream Velocity
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9 More Computational Fluid Dynamic Solutions Calculators
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Created Convection Resistance for Cylindrical Layer
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Created Heat Flow Rate through Cylindrical Composite Wall of 2 Layers
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Created Heat Flow Rate through Cylindrical Composite Wall of 3 Layers
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Created Heat Flow Rate through Cylindrical Wall
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Created Inner Surface Temperature of Cylindrical Wall in Conduction
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Created Length of Cylindrical Wall for given Heat Flow Rate
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Created Outer Surface Temperature of Cylindrical Composite Wall of 2 Layers
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Created Outer Surface Temperature of Cylindrical Wall given Heat Flow Rate
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Created Thermal Conductivity of Cylindrical Wall given Temperature Difference
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Created Thermal Resistance for Radial Heat Conduction in Cylinders
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Created Thickness of Cylindrical Wall to Maintain given Temperature Difference
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Created Total Thermal Resistance of 2 Cylindrical Resistances Connected in Series
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Created Total Thermal Resistance of 3 Cylindrical Resistances Connected in Series
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Created Total Thermal Resistance of Cylindrical Wall with Convection on Both Sides
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2 More Conduction in Cylinder Calculators
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Created Convection Resistance for Spherical Layer
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Created Heat Flow Rate through Spherical Composite Wall of 2 Layers in Series
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Created Heat Flow Rate through Spherical Wall
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Created Inner Surface Temperature of Spherical Wall
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Created Outer Surface Temperature of Spherical Wall
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Created Thermal Resistance of Spherical Composite Wall of 2 Layers in Series with Convection
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Created Thermal Resistance of Spherical Wall
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Created Thickness of Spherical Wall to Maintain given Temperature Difference
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Created Total Thermal Resistance of Spherical Wall of 2 Layers without Convection
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Created Total Thermal Resistance of Spherical wall of 3 Layers without Convection
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Created Total Thermal Resistance of Spherical Wall with Convection on Both Side
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Verified Location of Stagnation points for Rotating Cylinder in Uniform Flow Field
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Verified Radius of Cylinder for location of Stagnation Points
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5 More Cylinder Properties Calculators
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Verified Modified Radial Coordinate Equation for Cylindrical Blast Wave
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Verified Radial Coordinate of Cylindrical Blast Wave
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6 More Cylindrical Blast Wave Calculators
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Created Emissive Power given Radiation Intensity for Diffusely Emitting Surface
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Created Emissive power of diffusely emitted black body radiation given radiation intensity
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Created Intensity of diffusely emitted radiation given radiosity and reflected radiation
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Created Intensity of diffusely incident radiation given irradiation
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Created Intensity of diffusely reflected radiation given radiosity and emitted radiation
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Created Intensity of radiation emitted by black body at absolute temperature
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Created Irradiation for diffusely incident radiation
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Created Radiation intensity given emissive power for diffusely emitting black body
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Created Radiation intensity given emissive power for diffusely emitting surface
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Created Radiosity given incident and reflected radiation
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Created Temperature of diffusely emitting black body given radiation intensity
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Verified Diameter of Shaft for Speed and Shear Stress of Fluid in Journal Bearing
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Verified Diameter of Shaft for Torque Required in Foot-Step Bearing
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Verified External or Outer Radius of Collar for Total Torque
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Verified Internal or Inner Radius of Collar for Total Torque
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Verified Thickness of Oil Film for Shear Force in Journal Bearing
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Verified Thickness of Oil Film for Speed and Diameter of Shaft in Journal Bearing
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Verified Thickness of Oil Film for Torque required in Foot-Step Bearing
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12 More Dimensions and Geometry Calculators
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Verified Discharge over Broad-Crested Weir for Head of Liquid at Middle
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Verified Discharge over Broad-Crested Weir with Velocity of Approach
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Verified Discharge over Trapezoidal Notch or Weir
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Verified Discharge over Triangular Notch or Weir
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Verified Head of Liquid above V-notch
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Verified Time Required to Empty Tank with Triangular Weir or Notch
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11 More Discharge Calculators
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Verified Characteristic Mach Number behind Shock
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Verified Velocity behind Normal Shock
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13 More Downstream Shock Waves Calculators
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Verified Elastic Modulus of Composite in Transverse Direction
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5 More Elastic Modulus Calculators
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Verified Mean Free Path using Number Density
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Verified Molar Volume using Kinetic Energy per Mole
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Verified Number Density
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Verified Volume of Gas
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11 More Elements of Kinetic Theory Calculators
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Verified Density before Shock Formation for Expansion Wave
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Verified Ratio of New and Old Temperature for Expansion Waves
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Verified Temperature Ratio for Unsteady Expansion Wave
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2 More Expansion Waves Calculators
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Verified Difference of Pressure for Viscous or Laminar Flow
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Verified Power Absorbed in Collar Bearing
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Verified Power Absorbed in Foot-Step Bearing
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10 More Flow Analysis Calculators
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Verified Absolute pressure head at constant head and atmospheric pressure head
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Verified Atmospheric pressure head at constant head and absolute pressure head
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Verified Loss of head due to sudden enlargement
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3 More Flow Head Calculators
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Verified Area of Flow for Circular Channel
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Verified Chezy's constant considering Kutter's formula
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Verified Chezy's constant considering Manning's formula
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Verified Hydraulic mean depth considering Manning's formula
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Verified Manning's coefficient or constant
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Verified Radius of Circular Channel using Wetted Perimeter
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Verified Wetted Perimeter for Circular Channel
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12 More Flow in Open Channels Calculators
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Verified Coefficient of discharge
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Verified Coefficient of discharge for area and velocity
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Verified Coefficient of Discharge given Time for Emptying Tank
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8 More Flow Rate Calculators
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Verified Atmospheric pressure
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Verified Dynamic viscosity of electrolyte
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Verified Flow rate of electrolyte
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Verified Gap spacing
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Verified Pressure in flushing hole flow rate electrolyte
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Verified Radius of electrode
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Verified Radius of flushing hole
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Verified Velocity at section 2-2 for sudden contraction
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16 More Flow Regime Calculators
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Verified Rotational Speed for Torque Required in Collar Bearing
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Verified Rotational Speed for Torque Required in Foot-Step Bearing
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Verified Shear Force or Viscous Resistance in Journal Bearing
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Verified Speed of Rotation for Shear Force in Journal Bearing
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Verified Torque Required to Overcome Viscous Resistance in Collar Bearing
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Verified Torque Required to Overcome Viscous Resistance in Foot-Step Bearing
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15 More Fluid Flow and Resistance Calculators
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Created Force normal to shear force for given mean normal shear stress and area of shear plane
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3 More Force Normal to Shear Calculators
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Created Thermal Conductance for given Thermal Resistance
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Created Thermal resistance for conduction through 2 resistances in parallel
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Created Total Thermal Resistance for Conduction through Three Resistances in Series
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Created Total Thermal Resistance for Conduction through Two Resistances in Parallel
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Created Total Thermal Resistance for Conduction through Two Resistances in Series
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5 More Fundamental of Heat Transfer Calculators
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Verified Length of Weir for Broad-Crested Weir and Head of Liquid at Middle
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Verified Length of Weir for Broad-Crested Weir with Velocity of Approach
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8 More Geometric DImension Calculators
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Verified Area of Tank given Time for Emptying Tank
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7 More Geometric Dimensions Calculators
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Created Back Rake Angle for Orthogonal Cutting
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Created Cutting Speed
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Created Initial Diameter of Job in Turning
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Created Machine Feed
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Created Number of Jobs Revolution per Unit Time
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Created Uncut Chip Thickness
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4 More Geometry of Turning Process Calculators
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Verified Drag for given Glide Angle
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Verified Glide angle
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4 More Gliding Flight Calculators
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Created Radiation energy emitted by black body in time interval given emissive power
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Created Radiation energy emitted by black body in time interval given temperature
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Created Radiation energy emitted by black body per unit time and surface area
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Created Spectral black body emissive power Planck's law
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Created Surface Area of Black Body required to Emit certain amount of Radiation Energy
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Created Temperature of black body to emit certain amount of radiation energy
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Created Time required to emit specified amount of radiation energy from black body
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4 More Heat Emission due to Radiation Calculators
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Verified Lift Coefficient for given Turn Radius
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Verified Turn Rate for High Load Factor
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Verified Wing Loading for given Turn Rate
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14 More High Load Factor Maneuver Calculators
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Verified Radius of Curvature for Cylinder Wedge Body Shape
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Verified Radius of Curvature for Sphere Cone Body Shape
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7 More Hypersonic Flight Paths Velocity of Altitude Map Calculators
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Verified Doty and Rasmussen- Normal Force Coefficient
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Verified Rasmussen Closed Form Expression for Shock Wave Angle
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15 More Hypersonic Flow and Disturbances Calculators
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Verified Dimensions of Rankine half-body
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Verified Location of stagnation point on x-axis
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Verified Strength of source for Rankine half body
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Verified Uniform flow velocity for Rankine half body
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19 More Incompressible Flow Characteristics Calculators
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Verified Endurance of Jet Airplane
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Verified Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane
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15 More Jet Airplane Calculators
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Verified Angular Velocity of Vortex using Depth of Parabola
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Verified Depth of Parabola formed at Free Surface of Water
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Verified Rate of flow or discharge
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Verified Resultant velocity for two velocity components
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13 More Kinematics of Flow Calculators
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Created Absorptivity of Small Body using Absorbed Radiation and Temperature
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Created Emissivity of Small Body given Emitted Radiation and Temperature
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Created Radiation Absorbed by Small Body Per Unit of its Surface Area
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Created Radiation emitted by small body
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Created Temperature of Small Body given Emissivity and Emitted Radiation
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Created Temperature of Small Body using Absorptivity and Absorbed Radiation
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Verified Touchdown velocity for given stall velocity
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4 More Landing Calculators
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Verified Angle of Attack for Lift Coefficient on Airfoil
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Verified Circulation in Location of Stagnation Points
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Verified Coefficient of Lift for Airfoil
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13 More Lift and Circulation Calculators
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Verified Coefficient of Drag due to lift
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Verified Drag Coefficient for given parasite drag coefficient
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Verified Drag Coefficient for given zero-lift drag coefficient
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18 More Lift and Drag Polar Calculators
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Verified Coefficient of Drag due to Lift for Minimum Power required
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Verified Coefficient of Drag for given Thrust-to-Weight Ratio
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Verified Coefficient of Lift for given Thrust-to-Weight Ratio
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Verified Drag for Level and Unaccelerated Flight
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Verified Drag for Level and Unaccelerated Flight at Negligible Thrust Angle
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Verified Freestream Velocity given required Power
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Verified Freestream Velocity given Total Drag Force
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Verified Lift for Level and Unaccelerated Flight at Negligible Thrust Angle
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Verified Lift for Unaccelerated Flight
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Verified Zero-Lift Drag Coefficient for given Lift Coefficient
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Verified Zero-Lift Drag Coefficient for Minimum Power required
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8 More Lift and Drag Requirements Calculators
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Verified Diameter of Measuring Wires
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Verified Micrometer Measurement per Reading Lowenherz
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Verified Pitch Diameter Lowenherz
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Verified Pitch of Screw Lowenherz
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Verified Area of Cut from Tool Temperature
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Verified Cutting Speed from Tool Temperature
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Verified Specific Cutting Energy Per Unit Cutting Force from Tool Temperature
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Verified Specific Heat of Work from Tool Temperature
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Verified Thermal Conductivity of Work from Tool Temperature
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5 More Mechanics of Orthogonal Cutting Calculators
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Created Lead (approach or entering) angle for given side cutting edge angle
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Created Side cutting edge angle for given Lead (approach or entering) angle
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7 More Metal Cutting Tools Calculators
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Verified Diameter of Wire used in Three Wire System Method
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Verified Ideal wire diameter in three wire system method
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Verified Micrometer reading from three wire system method
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Verified Pitch diameter from three wire system method
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Verified Pitch of thread from three wire system method
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Verified Pitch of thread given ideal wire diameter
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Verified Thread Angle given Ideal Wire Diameter
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Verified Convective Heat Transfer to Surface
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1 More Modern Design Oriented Code Calculators
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Verified Molar Flux of Diffusing Component A through Non-Diffusing B based on Mole Fractions of A
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Verified Molar Flux of Diffusing Component A through Non-Diffusing B based on Partial Pressure of A
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15 More Molar Diffusion Calculators
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Verified Pressure at Inlet considering Maximum Flow Rate of Fluid
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Verified Pressure at Inlet of Tank or Vessel considering Compressible Fluid Flow
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5 More Multiphase Compressible Flow Calculators
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Verified Ambient atmospheric pressure
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Verified Net force acting on electrode
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Verified Pressure in flushing hole net force electrode
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Verified Coefficient of Drag Equation with Angle of Attack
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Verified Coefficient of Lift Equation with Angle of Attack
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Verified Drag Force with Angle of Attack
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Verified Lift Force with Angle of Attack
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10 More Newtonian Flow Calculators
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Verified Relation between Mach Number and Characteristic Mach Number
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6 More Normal Shock Relations Calculators
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Verified Component of Downstream Mach Normal to Oblique Shock
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Verified Flow Deflection Angle due to Oblique Shock
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8 More Oblique Shock Calculators
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Created Heat flow rate through pipe with eccentric lagging
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Created Heat flow through pipe in square section
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Created Inner surface temperature of pipe in square section
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Created Inner surface temperature of pipe with eccentric lagging
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Created Length of pipe with eccentric lagging
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Created Outer surface temperature of pipe in square section
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Created Outer surface temperature of pipe with eccentric lagging
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Created Thermal conductivity for pipe with eccentric lagging
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Created Thermal Resistance for Pipe in Square Section
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Created Thermal resistance of pipe with eccentric lagging
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1 More Other shapes Calculators
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Verified Overcut constant A
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Verified Overcut constant B
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Verified Overcut produced per side
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1 More Overcut Calculators
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Verified Blunt-Nosed Flat Plate Pressure Ratio (First Approximation)
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Verified Creation Pressure for Planar Blast Wave
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Verified Radial Coordinate for Planar Blast Wave
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5 More Planar and Blunt Slab Blast Wave Calculators
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Verified Loss of Head due to Sudden Contraction
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13 More Pressure and Flow Head Calculators
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Verified Atmospheric pressure at electrode tip
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Verified Pressure distribution in flushing gap
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Verified Pressure in flushing hole
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Verified Radial location of pressure distribution
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Verified Radius of electrode from pressure flushing hole
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Verified Radius of flushing hole EDM
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Verified Entropy Change across Normal Shock
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Verified Shock Strength
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4 More Property Change Across Shock Waves Calculators
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Verified Load Factor given Pull-Down Maneuver Rate
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Verified Load Factor given Pull-UP Maneuver Radius
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Verified Pull-Down Maneuver Rate
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Verified Pull-up maneuver radius
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Verified Velocity for given Turn Rate for High Load Factor
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7 More Pull Up and Pull Down Maneuver Calculators
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Verified Reynolds Number for Chord Length
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Verified Static Density of Plate using Chord Length for Flat Plate Case
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Verified Static Velocity of Plate using Chord Length for Flat Plate Case
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12 More Reference Temperature Method Calculators
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Created Mean normal stress in shear plane for given normal force and shear area
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5 More Resultants and Stress Calculators
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Verified Diameter of Wire used Sharp V
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Verified Micrometer Measurement per Reading Sharp V
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Verified Pitch Diameter Sharp V
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Verified Pitch of Screw Threads Sharp V
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Created Area of Plane Wall Required for Given Temperature Difference
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Created Inner Surface Temperature of Plane Wall
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Created Outer Surface Temperature of Wall in Conduction through Wall
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Created Temperature at Distance x from Inner Surface in Wall
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Created Thermal Conductivity of Material Required to Maintain Given Temperature Difference
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Created Thermal Resistance of Wall
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Created Thickness of Plane Wall for Conduction through Wall
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Created Total Thermal Resistance of Plane Wall with Convection on Both Sides
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Verified Enthalpy Equation using Specific Heat Ratio
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Verified Local Shock-Layer Thickness
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Verified Total Enthalpy Equation using Specific Heat Ratio and Velocities
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8 More Space Marching Finite Difference Method Additional Solutions of the Euler Equations Calculators
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Verified Density of Fluid for Stagnation considering Compressible Fluid Flow
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Verified Stagnation Density considering other Stagnation Properties of Fluid
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Verified Stagnation Density given Compressible Fluid Flow
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Verified Stagnation Pressure considering other Stagnation Properties of Fluid
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Verified Stagnation Pressure for Compressible Fluid Flow
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Verified Stagnation Temperature considering other Stagnation Properties of Fluid
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2 More Stagnation Properties Calculators
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Verified Static Temperature of Fluid over Flat Plate
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Verified Static Temperature of Plate using Wall Viscosity
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Verified Static Temperature over Flat Plate under Viscous, Very High Mach Flow
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3 More Static Parameters for Hypersonic Flow Calculators
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Verified Mach Number over Flat Plate using Static Temperature and Wall Temperature
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Verified Total Temperature over Flat Plate under Viscous Mach Flow
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Verified Total Temperature over Flat Plate under Viscous Very High Mach Flow
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5 More Supersonic Aerothermodynamics Calculators
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Verified Maximum Lift coefficient for given stall velocity
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Verified Stall velocity for given liftoff velocity
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13 More Take Off Calculators
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Verified Taper produced due to side sparks
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Verified Upper diameter of hole
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7 More Taper Formation Calculators
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Verified Minimum Thrust of aircraft required
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Verified Thrust Angle for Unaccelerated Level Flight for given Drag
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Verified Thrust Angle for Unaccelerated Level Flight for given Lift
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Verified Thrust for Level and Unaccelerated Flight
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Verified Thrust of Aircraft required for Level, Unaccelerated Flight
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Verified Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle
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Verified Weight of Aircraft in Level, Unaccelerated Flight
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12 More Thrust and Power Requirements Calculators
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Verified Tool temperature
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9 More Tool Life Calculators
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Verified Lift during level turn
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Verified Lift for given Load Factor
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Verified Load Factor given Turn Rate
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Verified Turn radius
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9 More Turning Flight Calculators
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Verified Diameter of wire used in measurement over wires method
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Verified Micrometer reading from measurement over wires method
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Verified Pitch diameter from measurement over wires method
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Verified Pitch of thread from measurement over wires method
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Verified Best size wire
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Verified Best wire size for modified buttress 45deg and 7deg
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Verified Micrometer reading per measurement
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Verified Pitch diameter unsymmetrical threads
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Verified Pitch for modified buttress 45deg and 7deg
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Verified Pitch of Screw Unsymmetrical Threads
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Verified Coefficient of velocity for horizontal and vertical distance
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Verified Time of Emptying Tank through Orifice at Bottom
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Verified Velocity of liquid at C-C for Hc, Ha, and H
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5 More Velocity and Time Calculators
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Verified Wall Temperature of Fluid over Flat Plate
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Verified Wall Temperature of Plate using Wall Viscosity
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2 More Wall Temperature Calculators
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Verified Volume of electrode material worn out
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Verified Volume of work material removed
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Verified Wear Ratio
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Verified Diameter of Wire
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Verified Micrometer Reading per Measurement Whitworth
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Verified Pitch diameter whitworth
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Verified pitch of screw threads whitworth
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Verified Angle of Attack of Wing
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14 More Wing Tail Contribution Calculators
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