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Calculators Created by Sai Venkata Phanindra Chary Arendra
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
89
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 89 different categories till date.
Charging Current for EDM
(5)
Verified
Charging Current in Relaxation Circuit
Go
Verified
Power Supply during Charging
Go
Verified
Resistance of Charging Circuit
Go
Verified
Time Constant from Charging Current
Go
Verified
Time Elapsed during Charging
Go
2 Layers
(8)
Created
Area of Composite Wall of 2 Layers
Go
Created
Heat Flow Rate through Composite Wall of 2 Layers in Series
Go
Created
Inner Surface Temperature of Composite Wall for 2 Layers in Series
Go
Created
Interface Temperature of Composite Wall of 2 Layers given Inner Surface Temperature
Go
Created
Interface Temperature of Composite Wall of 2 Layers given Outer Surface Temperature
Go
Created
Length of 2nd Layer of Composite Wall in Conduction through Walls
Go
Created
Outer Surface Temperature of Composite Wall of 2 Layers for Conduction
Go
Created
Thermal Resistance of Composite Wall with 2 Layers in Series
Go
3 Layers
(6)
Created
Area of Composite Wall of 3 Layers
Go
Created
Heat Flow Rate through Composite Wall of 3 Layers in Series
Go
Created
Inner Surface Temperature of Composite Wall of 3 Layers in Series
Go
Created
Length of 3rd Layer of Composite Wall in Conduction through Walls
Go
Created
Outer Surface Temperature of Composite Wall of 3 Layers for Conduction
Go
Created
Thermal Resistance of Composite Wall with 3 Layers in Series
Go
Absorptivity, Reflectivity and Transmissivity
(18)
Created
Absorbed Radiation using Absorptivity and Incident Radiation
Go
Created
Absorbed Radiation using Incident, Reflected and Transmitted Radiation
Go
Created
Absorptivity
Go
Created
Absorptivity using Reflectivity and Transmissivity
Go
Created
Absorptivity using Reflectivity for Opaque Surface
Go
Created
Incident Radiation given Reflectivity and Reflected Radiation
Go
Created
Incident Radiation using Absorbed, Reflected and Transmitted Radiation
Go
Created
Incident Radiation using Absorptivity and Absorbed Energy
Go
Created
Incident Radiation using Transmissivity and Transmitted Radiation
Go
Created
Reflected Radiation given Incident, Absorbed and Transmitted Radiation
Go
Created
Reflected Radiation given Reflectivity and Incident Radiation
Go
Created
Reflectivity given Absorptivity and Transmissivity
Go
Created
Reflectivity using Absorptivity for Opaque Surface
Go
Created
Reflectivity using Reflected Radiation and Incident Radiation
Go
Created
Transmissivity given Transmitted Radiation and Incident Radiation
Go
Created
Transmissivity using Absorptivity and Reflectivity
Go
Created
Transmitted Radiation using Incident, Absorbed and Reflected Radiation
Go
Created
Transmitted Radiation using Transmissivity and Incident Radiation
Go
ACME Thread
(4)
Verified
Diameter of measuring wires ACME threads
Go
Verified
Micrometer measurement per reading acme threads
Go
Verified
Pitch diameter acme threads
Go
Verified
Pitch of screw acme threads
Go
Aero-Thermal Dynamics
(4)
Verified
Internal Energy for Hypersonic Flow
Go
Verified
Non Dimensional Internal Energy Parameter
Go
Verified
Static Enthalpy
Go
Verified
Wall Temperature Calculation using Internal Energy Change
Go
12 More Aero-Thermal Dynamics Calculators
Go
Approximate Methods of Hypersonic Inviscid Flowfields
(2)
Verified
Non-Dimensional Radius for Hypersonic Vehicles
Go
Verified
Transformed Conical Variable
Go
9 More Approximate Methods of Hypersonic Inviscid Flowfields Calculators
Go
Approximate Results Applied to Hypersonic Vehicles
(6)
Verified
Free Stream Enthalpy over Flat Plate with Freestream Conditions
Go
Verified
Free Stream Velocity over Flat Plate using Drag Force
Go
Verified
Free Stream Velocity over Flat Plate with Freestream Conditions
Go
Verified
Freestream Density over Flat under Freestream Flow Conditions
Go
Verified
Pressure Ratio for Insulated Flat Plate, Strong Interaction
Go
Verified
Total Enthalpy over Flat Plate with Freestream Conditions
Go
9 More Approximate Results Applied to Hypersonic Vehicles Calculators
Go
Atmospheric and Solar Radiation
(6)
Created
Diffuse solar radiation given total solar energy and direct radiation
Go
Created
Effective surface temperature of sun given solar constant
Go
Created
Mean distance between sun or star and earth or planet
Go
Created
Radius of sun given total solar irradiance
Go
Created
Total solar energy incident on unit area of horizontal surface on ground
Go
Created
Total solar irradiance or solar constant
Go
Basics of HMT
(5)
Created
Thermal Conductance for given Thermal Resistance
Go
Created
Thermal resistance for conduction through 2 resistances in parallel
Go
Created
Total Thermal Resistance for Conduction through Three Resistances in Series
Go
Created
Total Thermal Resistance for Conduction through Two Resistances in Parallel
Go
Created
Total Thermal Resistance for Conduction through Two Resistances in Series
Go
1 More Basics of HMT Calculators
Go
British Association Thread
(4)
Verified
Diameter of measuring wires British threads
Go
Verified
Micrometer measurement per reading British threads
Go
Verified
Pitch diameter British thread
Go
Verified
Pitch of screw British
Go
Buoyancy
(2)
Verified
Time Period of Oscillation of Ship
Go
Verified
Volume of body in fluid for metacentric height and BG
Go
9 More Buoyancy Calculators
Go
Clearance fits
(1)
Verified
Tolerance Unit
Go
6 More Clearance fits Calculators
Go
Climbing Flight
(8)
Verified
Centrifugal Force in Accelerated Flight
Go
Verified
Drag in Accelerated Flight
Go
Verified
Excess power for given rate of climb
Go
Verified
Lift in Accelerated Flight
Go
Verified
Thrust in Accelerated Flight
Go
Verified
Velocity in Accelerated Flight
Go
Verified
Velocity of aircraft at given rate of climb
Go
Verified
Velocity of aircraft for given excess power
Go
8 More Climbing Flight Calculators
Go
Compressible Flow Parameters
(3)
Verified
Mach Number for Compressible Fluid Flow
Go
Verified
Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid
Go
Verified
Velocity of Sound Wave given Mach Number for Compressible Fluid Flow
Go
7 More Compressible Flow Parameters Calculators
Go
Compression Waves
(1)
Verified
New Pressure after Shock Formation for Compression Wave
Go
2 More Compression Waves Calculators
Go
Computational Fluid Dynamic Solutions
(2)
Verified
Freestream Density
Go
Verified
Freestream Velocity
Go
9 More Computational Fluid Dynamic Solutions Calculators
Go
Conduction in Cylinder
(14)
Created
Convection Resistance for Cylindrical Layer
Go
Created
Heat Flow Rate through Cylindrical Composite Wall of 2 Layers
Go
Created
Heat Flow Rate through Cylindrical Composite Wall of 3 Layers
Go
Created
Heat Flow Rate through Cylindrical Wall
Go
Created
Inner Surface Temperature of Cylindrical Wall in Conduction
Go
Created
Length of Cylindrical Wall for given Heat Flow Rate
Go
Created
Outer Surface Temperature of Cylindrical Composite Wall of 2 Layers
Go
Created
Outer Surface Temperature of Cylindrical Wall given Heat Flow Rate
Go
Created
Thermal Conductivity of Cylindrical Wall given Temperature Difference
Go
Created
Thermal Resistance for Radial Heat Conduction in Cylinders
Go
Created
Thickness of Cylindrical Wall to Maintain given Temperature Difference
Go
Created
Total Thermal Resistance of 2 Cylindrical Resistances Connected in Series
Go
Created
Total Thermal Resistance of 3 Cylindrical Resistances Connected in Series
Go
Created
Total Thermal Resistance of Cylindrical Wall with Convection on Both Sides
Go
Conduction in Plane Wall
(8)
Created
Area of Plane Wall Required for Given Temperature Difference
Go
Created
Inner Surface Temperature of Plane Wall
Go
Created
Outer Surface Temperature of Wall in Conduction through Wall
Go
Created
Temperature at Distance x from Inner Surface in Wall
Go
Created
Thermal Conductivity of Material Required to Maintain Given Temperature Difference
Go
Created
Thermal Resistance of Wall
Go
Created
Thickness of Plane Wall for Conduction through Wall
Go
Created
Total Thermal Resistance of Plane Wall with Convection on Both Sides
Go
Conduction in Sphere
(11)
Created
Convection Resistance for Spherical Layer
Go
Created
Heat Flow Rate through Spherical Composite Wall of 2 Layers in Series
Go
Created
Heat Flow Rate through Spherical Wall
Go
Created
Inner Surface Temperature of Spherical Wall
Go
Created
Outer Surface Temperature of Spherical Wall
Go
Created
Thermal Resistance of Spherical Composite Wall of 2 Layers in Series with Convection
Go
Created
Thermal Resistance of Spherical Wall
Go
Created
Thickness of Spherical Wall to Maintain given Temperature Difference
Go
Created
Total Thermal Resistance of Spherical Wall of 2 Layers without Convection
Go
Created
Total Thermal Resistance of Spherical wall of 3 Layers without Convection
Go
Created
Total Thermal Resistance of Spherical Wall with Convection on Both Side
Go
Cylinder Properties
(2)
Verified
Location of Stagnation points for Rotating Cylinder in Uniform Flow Field
Go
Verified
Radius of Cylinder for location of Stagnation Points
Go
5 More Cylinder Properties Calculators
Go
Cylindrical Blast Wave
(2)
Verified
Modified Radial Coordinate Equation for Cylindrical Blast Wave
Go
Verified
Radial Coordinate of Cylindrical Blast Wave
Go
6 More Cylindrical Blast Wave Calculators
Go
Diffuse Radiation
(11)
Created
Emissive Power given Radiation Intensity for Diffusely Emitting Surface
Go
Created
Emissive power of diffusely emitted black body radiation given radiation intensity
Go
Created
Intensity of diffusely emitted radiation given radiosity and reflected radiation
Go
Created
Intensity of diffusely incident radiation given irradiation
Go
Created
Intensity of diffusely reflected radiation given radiosity and emitted radiation
Go
Created
Intensity of radiation emitted by black body at absolute temperature
Go
Created
Irradiation for diffusely incident radiation
Go
Created
Radiation intensity given emissive power for diffusely emitting black body
Go
Created
Radiation intensity given emissive power for diffusely emitting surface
Go
Created
Radiosity given incident and reflected radiation
Go
Created
Temperature of diffusely emitting black body given radiation intensity
Go
Dimensions and Geometry
(7)
Verified
Diameter of Shaft for Speed and Shear Stress of Fluid in Journal Bearing
Go
Verified
Diameter of Shaft for Torque Required in Foot-Step Bearing
Go
Verified
External or Outer Radius of Collar for Total Torque
Go
Verified
Internal or Inner Radius of Collar for Total Torque
Go
Verified
Thickness of Oil Film for Shear Force in Journal Bearing
Go
Verified
Thickness of Oil Film for Speed and Diameter of Shaft in Journal Bearing
Go
Verified
Thickness of Oil Film for Torque required in Foot-Step Bearing
Go
12 More Dimensions and Geometry Calculators
Go
Discharge
(6)
Verified
Discharge over Broad-Crested Weir for Head of Liquid at Middle
Go
Verified
Discharge over Broad-Crested Weir with Velocity of Approach
Go
Verified
Discharge over Trapezoidal Notch or Weir
Go
Verified
Discharge over Triangular Notch or Weir
Go
Verified
Head of Liquid above V-notch
Go
Verified
Time Required to Empty Tank with Triangular Weir or Notch
Go
11 More Discharge Calculators
Go
Downstream Shock Waves
(2)
Verified
Characteristic Mach Number behind Shock
Go
Verified
Velocity behind Normal Shock
Go
13 More Downstream Shock Waves Calculators
Go
Elastic Modulus
(1)
Verified
Elastic Modulus of Composite in Transverse Direction
Go
5 More Elastic Modulus Calculators
Go
Elements of Kinetic Theory
(4)
Verified
Mean Free Path using Number Density
Go
Verified
Molar Volume using Kinetic Energy per Mole
Go
Verified
Number Density
Go
Verified
Volume of Gas
Go
11 More Elements of Kinetic Theory Calculators
Go
Expansion Waves
(3)
Verified
Density before Shock Formation for Expansion Wave
Go
Verified
Ratio of New and Old Temperature for Expansion Waves
Go
Verified
Temperature Ratio for Unsteady Expansion Wave
Go
2 More Expansion Waves Calculators
Go
Flow Analysis
(3)
Verified
Difference of Pressure for Viscous or Laminar Flow
Go
Verified
Power Absorbed in Collar Bearing
Go
Verified
Power Absorbed in Foot-Step Bearing
Go
10 More Flow Analysis Calculators
Go
Flow Head
(3)
Verified
Absolute pressure head at constant head and atmospheric pressure head
Go
Verified
Atmospheric pressure head at constant head and absolute pressure head
Go
Verified
Loss of head due to sudden enlargement
Go
3 More Flow Head Calculators
Go
Flow in Open Channels
(7)
Verified
Area of Flow for Circular Channel
Go
Verified
Chezy's constant considering Kutter's formula
Go
Verified
Chezy's constant considering Manning's formula
Go
Verified
Hydraulic mean depth considering Manning's formula
Go
Verified
Manning's coefficient or constant
Go
Verified
Radius of Circular Channel using Wetted Perimeter
Go
Verified
Wetted Perimeter for Circular Channel
Go
12 More Flow in Open Channels Calculators
Go
Flow Rate
(3)
Verified
Coefficient of discharge
Go
Verified
Coefficient of discharge for area and velocity
Go
Verified
Coefficient of Discharge given Time for Emptying Tank
Go
8 More Flow Rate Calculators
Go
Flow rate of the electrolyte
(7)
Verified
Atmospheric pressure
Go
Verified
Dynamic viscosity of electrolyte
Go
Verified
Flow rate of electrolyte
Go
Verified
Gap spacing
Go
Verified
Pressure in flushing hole flow rate electrolyte
Go
Verified
Radius of electrode
Go
Verified
Radius of flushing hole
Go
Flow Regime
(1)
Verified
Velocity at section 2-2 for sudden contraction
Go
16 More Flow Regime Calculators
Go
Fluid Flow and Resistance
(6)
Verified
Rotational Speed for Torque Required in Collar Bearing
Go
Verified
Rotational Speed for Torque Required in Foot-Step Bearing
Go
Verified
Shear Force or Viscous Resistance in Journal Bearing
Go
Verified
Speed of Rotation for Shear Force in Journal Bearing
Go
Verified
Torque Required to Overcome Viscous Resistance in Collar Bearing
Go
Verified
Torque Required to Overcome Viscous Resistance in Foot-Step Bearing
Go
15 More Fluid Flow and Resistance Calculators
Go
Force Normal to Shear
(1)
Created
Force normal to shear force for given mean normal shear stress and area of shear plane
Go
3 More Force Normal to Shear Calculators
Go
Geometric DImension
(2)
Verified
Length of Weir for Broad-Crested Weir and Head of Liquid at Middle
Go
Verified
Length of Weir for Broad-Crested Weir with Velocity of Approach
Go
8 More Geometric DImension Calculators
Go
Geometric Dimensions
(1)
Verified
Area of Tank given Time for Emptying Tank
Go
7 More Geometric Dimensions Calculators
Go
Geometry of Turning Process
(6)
Created
Back Rake Angle for Orthogonal Cutting
Go
Created
Cutting Speed
Go
Created
Initial Diameter of Job in Turning
Go
Created
Machine Feed
Go
Created
Number of Jobs Revolution per Unit Time
Go
Created
Uncut Chip Thickness
Go
4 More Geometry of Turning Process Calculators
Go
Gliding Flight
(2)
Verified
Drag for given Glide Angle
Go
Verified
Glide angle
Go
4 More Gliding Flight Calculators
Go
High Load Factor Maneuver
(8)
Verified
Lift Coefficient for given Turn Radius
Go
Verified
Load Factor given Pull-down Maneuver Rate
Go
Verified
Load Factor given Pull-UP Maneuver Radius
Go
Verified
Pull-down maneuver rate
Go
Verified
Pull-up maneuver radius
Go
Verified
Turn rate for high load factor
Go
Verified
Velocity for given turn rate for high load factor
Go
Verified
Wing loading for given turn rate
Go
21 More High Load Factor Maneuver Calculators
Go
Hypersonic Flight Paths Velocity of Altitude Map
(2)
Verified
Radius of Curvature for Cylinder Wedge Body Shape
Go
Verified
Radius of Curvature for Sphere Cone Body Shape
Go
7 More Hypersonic Flight Paths Velocity of Altitude Map Calculators
Go
Hypersonic Flow and Shock Wave Dynamics
(2)
Verified
Doty and Rasmussen- Normal Force Coefficient
Go
Verified
Rasmussen Closed Form Expression for Shock Wave Angle
Go
10 More Hypersonic Flow and Shock Wave Dynamics Calculators
Go
Incompressible Flow Characteristics
(4)
Verified
Dimensions of Rankine half-body
Go
Verified
Location of stagnation point on x-axis
Go
Verified
Strength of source for Rankine half body
Go
Verified
Uniform flow velocity for Rankine half body
Go
19 More Incompressible Flow Characteristics Calculators
Go
Jet Airplane
(2)
Verified
Endurance of Jet Airplane
Go
Verified
Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane
Go
16 More Jet Airplane Calculators
Go
Kinematics of Flow
(4)
Verified
Angular Velocity of Vortex using Depth of Parabola
Go
Verified
Depth of Parabola formed at Free Surface of Water
Go
Verified
Rate of flow or discharge
Go
Verified
Resultant velocity for two velocity components
Go
13 More Kinematics of Flow Calculators
Go
Kirchhoff's Law
(6)
Created
Absorptivity of Small Body using Absorbed Radiation and Temperature
Go
Created
Emissivity of Small Body given Emitted Radiation and Temperature
Go
Created
Radiation Absorbed by Small Body Per Unit of its Surface Area
Go
Created
Radiation emitted by small body
Go
Created
Temperature of Small Body given Emissivity and Emitted Radiation
Go
Created
Temperature of Small Body using Absorptivity and Absorbed Radiation
Go
Landing
(1)
Verified
Touchdown velocity for given stall velocity
Go
4 More Landing Calculators
Go
Lift and Circulation
(3)
Verified
Angle of Attack for Lift Coefficient on Airfoil
Go
Verified
Circulation in Location of Stagnation Points
Go
Verified
Coefficient of Lift for Airfoil
Go
13 More Lift and Circulation Calculators
Go
Lift and Drag Polar
(3)
Verified
Coefficient of Drag due to lift
Go
Verified
Drag Coefficient for given parasite drag coefficient
Go
Verified
Drag Coefficient for given zero-lift drag coefficient
Go
18 More Lift and Drag Polar Calculators
Go
Lift and Drag Requirements
(11)
Verified
Coefficient of Drag due to lift for minimum power required
Go
Verified
Coefficient of Drag for given thrust-to-weight ratio
Go
Verified
Coefficient of Lift for given thrust-to-weight ratio
Go
Verified
Drag for Level and Unaccelerated Flight
Go
Verified
Drag for Level and Unaccelerated Flight at Negligible Thrust Angle
Go
Verified
Freestream velocity for given required power
Go
Verified
Freestream Velocity for given total drag force
Go
Verified
Lift for Level and Unaccelerated Flight at Negligible Thrust Angle
Go
Verified
Lift for Unaccelerated Flight
Go
Verified
Zero-lift drag coefficient for given lift coefficient
Go
Verified
Zero-lift drag coefficient for minimum power required
Go
8 More Lift and Drag Requirements Calculators
Go
Lowenherz Thread
(4)
Verified
Diameter of measuring wires
Go
Verified
Micrometer measurement per reading lowenherz
Go
Verified
Pitch diameter lowenherz
Go
Verified
Pitch of screw lowenherz
Go
Mechanics of Orthogonal Cutting
(5)
Verified
Area of Cut from Tool Temperature
Go
Verified
Cutting Speed from Tool Temperature
Go
Verified
Specific Cutting Energy Per Unit Cutting Force from Tool Temperature
Go
Verified
Specific Heat of Work from Tool Temperature
Go
Verified
Thermal Conductivity of Work from Tool Temperature
Go
5 More Mechanics of Orthogonal Cutting Calculators
Go
Metal Cutting Tools
(2)
Created
Lead (approach or entering) angle for given side cutting edge angle
Go
Created
Side cutting edge angle for given Lead (approach or entering) angle
Go
7 More Metal Cutting Tools Calculators
Go
Metric Thread
(7)
Verified
Diameter of wire used in three wire system method
Go
Verified
Ideal wire diameter in three wire system method
Go
Verified
Micrometer reading from three wire system method
Go
Verified
Pitch diameter from three wire system method
Go
Verified
Pitch of thread from three wire system method
Go
Verified
Pitch of thread given ideal wire diameter
Go
Verified
Thread angle given ideal wire diameter
Go
Modern Design Oriented Code
(1)
Verified
Convective Heat Transfer to Surface
Go
1 More Modern Design Oriented Code Calculators
Go
Molar Diffusion
(2)
Verified
Molar Flux of Diffusing Component A through Non-Diffusing B based on Mole Fractions of A
Go
Verified
Molar Flux of Diffusing Component A through Non-Diffusing B based on Partial Pressure of A
Go
15 More Molar Diffusion Calculators
Go
Multiphase Compressible Flow
(2)
Verified
Pressure at Inlet considering Maximum Flow Rate of Fluid
Go
Verified
Pressure at Inlet of Tank or Vessel considering Compressible Fluid Flow
Go
5 More Multiphase Compressible Flow Calculators
Go
Net force acting on the electrode
(3)
Verified
Ambient atmospheric pressure
Go
Verified
Net force acting on electrode
Go
Verified
Pressure in flushing hole net force electrode
Go
Newtonian Flow
(4)
Verified
Coefficient of Drag Equation with Angle of Attack
Go
Verified
Coefficient of Lift Equation with Angle of Attack
Go
Verified
Drag Force with Angle of Attack
Go
Verified
Lift Force with Angle of Attack
Go
10 More Newtonian Flow Calculators
Go
Normal Shock Relations
(1)
Verified
Relation between Mach Number and Characteristic Mach Number
Go
6 More Normal Shock Relations Calculators
Go
Oblique Shock
(2)
Verified
Component of Downstream Mach Normal to Oblique Shock
Go
Verified
Flow Deflection Angle due to Oblique Shock
Go
8 More Oblique Shock Calculators
Go
Other shapes
(10)
Created
Heat flow rate through pipe with eccentric lagging
Go
Created
Heat flow through pipe in square section
Go
Created
Inner surface temperature of pipe in square section
Go
Created
Inner surface temperature of pipe with eccentric lagging
Go
Created
Length of pipe with eccentric lagging
Go
Created
Outer surface temperature of pipe in square section
Go
Created
Outer surface temperature of pipe with eccentric lagging
Go
Created
Thermal conductivity for pipe with eccentric lagging
Go
Created
Thermal Resistance for Pipe in Square Section
Go
Created
Thermal resistance of pipe with eccentric lagging
Go
1 More Other shapes Calculators
Go
Overcut
(3)
Verified
Overcut constant A
Go
Verified
Overcut constant B
Go
Verified
Overcut produced per side
Go
1 More Overcut Calculators
Go
Planar and Blunt Slab Blast Wave
(3)
Verified
Blunt-Nosed Flat Plate Pressure Ratio (First Approximation)
Go
Verified
Creation Pressure for Planar Blast Wave
Go
Verified
Radial Coordinate for Planar Blast Wave
Go
5 More Planar and Blunt Slab Blast Wave Calculators
Go
Pressure and Flow Head
(1)
Verified
Loss of Head due to Sudden Contraction
Go
13 More Pressure and Flow Head Calculators
Go
Pressure distribution in the flushing gap
(6)
Verified
Atmospheric pressure at electrode tip
Go
Verified
Pressure distribution in flushing gap
Go
Verified
Pressure in flushing hole
Go
Verified
Radial location of pressure distribution
Go
Verified
Radius of electrode from pressure flushing hole
Go
Verified
Radius of flushing hole EDM
Go
Property Change Across Shock Waves
(2)
Verified
Entropy Change across Normal Shock
Go
Verified
Shock Strength
Go
4 More Property Change Across Shock Waves Calculators
Go
Radiation
(7)
Created
Radiation energy emitted by black body in time interval given emissive power
Go
Created
Radiation energy emitted by black body in time interval given temperature
Go
Created
Radiation energy emitted by black body per unit time and surface area
Go
Created
Spectral black body emissive power Planck's law
Go
Created
Surface Area of Black Body required to Emit certain amount of Radiation Energy
Go
Created
Temperature of black body to emit certain amount of radiation energy
Go
Created
Time required to emit specified amount of radiation energy from black body
Go
1 More Radiation Calculators
Go
Reference Temperature Method
(3)
Verified
Reynolds Number for Chord Length
Go
Verified
Static Density of Plate using Chord Length for Flat Plate Case
Go
Verified
Static Velocity of Plate using Chord Length for Flat Plate Case
Go
12 More Reference Temperature Method Calculators
Go
Resultants and Stress
(1)
Created
Mean normal stress in shear plane for given normal force and shear area
Go
5 More Resultants and Stress Calculators
Go
Sharp-V Thread
(4)
Verified
Diameter of wire used Sharp V
Go
Verified
Micrometer measurement per reading sharp V
Go
Verified
Pitch diameter sharp v
Go
Verified
Pitch of screw threads sharp v
Go
Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations
(3)
Verified
Enthalpy Equation using Specific Heat Ratio
Go
Verified
Local Shock-Layer Thickness
Go
Verified
Total Enthalpy Equation using Specific Heat Ratio and Velocities
Go
8 More Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations Calculators
Go
Stagnation Properties
(6)
Verified
Density of Fluid for Stagnation considering Compressible Fluid Flow
Go
Verified
Stagnation Density considering other Stagnation Properties of Fluid
Go
Verified
Stagnation Density given Compressible Fluid Flow
Go
Verified
Stagnation Pressure considering other Stagnation Properties of Fluid
Go
Verified
Stagnation Pressure for Compressible Fluid Flow
Go
Verified
Stagnation Temperature considering other Stagnation Properties of Fluid
Go
2 More Stagnation Properties Calculators
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Static Parameters for Hypersonic Flow
(3)
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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Supersonic Aerothermodynamics
(3)
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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Take-Off
(2)
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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Taper Formation
(2)
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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Thrust and Power Requirements
(7)
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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Tool Life
(1)
Verified
Tool temperature
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9 More Tool Life Calculators
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Turning Flight
(4)
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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Two Wires System Method
(4)
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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Unsymmetrical threads
(6)
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
Go
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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Velocity and Time
(3)
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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Wall Temperature
(2)
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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Wear Ratio
(3)
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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Whitworth Thread
(4)
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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Wing-Tail Contribution
(1)
Verified
Angle of attack of wing
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14 More Wing-Tail Contribution Calculators
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