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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
121
Formulas Created
254
Formulas Verified
73
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 121 and verified 254 calculators across 73 different categories till date.
Absorptivity, Reflectivity and Transmissivity
(18)
Created
Absorbed radiation in terms of absorptivity and incident radiation
Go
Created
Absorbed radiation in terms of incident, reflected and transmitted radiation
Go
Created
Absorptivity
Go
Created
Absorptivity in terms of reflectivity and transmissivity
Go
Created
Absorptivity in terms of reflectivity for opaque surface
Go
Created
Incident radiation in terms of absorbed, reflected and transmitted radiation
Go
Created
Incident radiation in terms of absorptivity and absorbed energy
Go
Created
Incident radiation in terms of reflectivity and reflected radiation
Go
Created
Incident radiation in terms of transmissivity and transmitted radiation
Go
Created
Reflected radiation in terms of incident, absorbed and transmitted radiation
Go
Created
Reflected radiation in terms of reflectivity and incident radiation
Go
Created
Reflectivity in terms of absorptivity and transmissivity
Go
Created
Reflectivity in terms of absorptivity for opaque surface
Go
Created
Reflectivity in terms of reflected radiation and incident radiation
Go
Created
Transmissivity in terms of absorptivity and reflectivity
Go
Created
Transmissivity in terms of transmitted radiation and incident radiation
Go
Created
Transmitted radiation in terms of incident, absorbed and reflected radiation
Go
Created
Transmitted radiation in terms of transmissivity and incident radiation
Go
ACME Threads 29deg. included angle
(4)
Verified
Diameter of the measuring wires ACME threads
Go
Verified
Micrometer measurement/reading acme threads
Go
Verified
Pitch diameter acme threads
Go
Verified
Pitch of screw acme threads
Go
Approximate Results Applied to Hypersonic Vehicles
(6)
Verified
Free stream enthalpy over a flat plate with freestream conditions
Go
Verified
Free stream velocity over a flat plate using drag force
Go
Verified
Free stream velocity over a flat plate with freestream conditions
Go
Verified
Freestream density over the flat under the freestream flow conditions
Go
Verified
Insulated flat plate, the strong interaction
Go
Verified
Total enthalpy over a 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 in terms of total solar energy and direct radiation
Go
Created
Effective surface temperature of the sun in terms of solar constant
Go
Created
Mean distance between sun/star and earth/planet
Go
Created
Radius of the sun in terms of total solar irradiance
Go
Created
Total solar energy incident on the unit area of a horizontal surface on the ground
Go
Created
Total solar irradiance or solar constant
Go
Basics
(1)
Created
Thermal resistance for conduction through 2 resistances in parallel
Go
6 More Basics Calculators
Go
Basics
(4)
Created
Thermal conductance for given thermal resistance
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 Calculators
Go
British association 47 and 1/2deg included angle
(4)
Verified
Diameter of the measuring wires British threads
Go
Verified
Micrometer measurement/reading British threads
Go
Verified
Pitch diameter British thread
Go
Verified
pitch of screw British
Go
Buoyancy
(2)
Verified
Time period of oscillation in the ship
Go
Verified
Volume of body in fluid for metacentric height and BG
Go
7 More Buoyancy Calculators
Go
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
Compressible flow
(11)
Verified
Density of the fluid for stagnation considering compressible fluid flow
Go
Verified
Mach number for the compressible fluid flow
Go
Verified
Pressure at inlet considering maximum flow rate of fluid
Go
Verified
Pressure at inlet of the tank or vessel considering compressible fluid flow
Go
Verified
Stagnation density considering other stagnation properties of the fluid
Go
Verified
Stagnation density considering the compressible fluid flow
Go
Verified
Stagnation pressure considering other stagnation properties of the fluid
Go
Verified
Stagnation pressure for the compressible fluid flow
Go
Verified
Stagnation temperature considering other stagnation properties of the fluid
Go
Verified
Velocity at the outlet of the nozzle for maximum flow rate of fluid
Go
Verified
Velocity of sound wave in Mach number for the compressible fluid flow
Go
13 More Compressible flow Calculators
Go
COMPUTATIONAL-FLUID-DYNAMIC SOLUTIONS
(2)
Verified
Freestream density
Go
Verified
Freestream velocity
Go
2 More COMPUTATIONAL-FLUID-DYNAMIC SOLUTIONS Calculators
Go
Cylinders
(14)
Created
Convection resistance for a cylindrical layer
Go
Created
Heat flow rate through a cylindrical composite wall of 2 layers
Go
Created
Heat flow rate through a cylindrical composite wall of 3 layers
Go
Created
Heat flow rate through a cylindrical wall
Go
Created
Inner surface temperature of a cylindrical wall for a given heat flow rate
Go
Created
Length of the cylindrical wall for a given heat flow rate
Go
Created
Outer surface temperature of a cylindrical wall for a given heat flow rate
Go
Created
Outer surface temperature of the cylindrical composite wall of 2 layers
Go
Created
Thermal conductivity of a cylindrical wall for a given temperature difference
Go
Created
Thermal resistance for radial heat conduction offered by a cylinder wall
Go
Created
Thickness of the cylindrical wall to maintain a 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 a cylindrical wall with convection either side
Go
Diffuse radiation
(11)
Created
Emissive power in terms of radiation intensity for diffusely emitting surface
Go
Created
Emissive power of diffusely emitted black body radiation in terms of radiation intensity
Go
Created
Intensity of diffusely emitted radiation in terms of radiosity and reflected radiation
Go
Created
Intensity of diffusely incident radiation in terms of irradiation
Go
Created
Intensity of diffusely reflected radiation in terms of radiosity and emitted radiation
Go
Created
Irradiation for a diffusely incident radiation
Go
Created
Radiation intensity in terms of emissive power for diffusely emitting black body
Go
Created
Radiation intensity in terms of emissive power for diffusely emitting surface
Go
Created
Radiosity in terms of incident and reflected radiation
Go
Created
Temperature of a diffusely emitting black body in terms of radiation intensity
Go
Created
The intensity of radiation emitted by a black body at an absolute temperature
Go
Drag during Level Unaccelerated Flight
(3)
Verified
Coefficient of Drag for given thrust-to-weight ratio
Go
Verified
Drag for a level, unaccelerated flight at negligible thrust angle
Go
Verified
Zero-lift drag coefficient for given lift coefficient
Go
4 More Drag during Level Unaccelerated Flight 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
Equations of Motion
(11)
Verified
Centrifugal Force in an accelerated flight
Go
Verified
Drag for a level, unaccelerated flight
Go
Verified
Drag in an accelerated flight
Go
Verified
Lift for an unaccelerated flight
Go
Verified
Lift in an accelerated flight
Go
Verified
Thrust angle for an unaccelerated flight for given drag
Go
Verified
Thrust angle for an unaccelerated flight for given lift
Go
Verified
Thrust for a level, unaccelerated flight
Go
Verified
Thrust in an accelerated flight
Go
Verified
Velocity in an accelerated flight
Go
Verified
Weight of aircraft in level, unaccelerated flight
Go
Flight Envelope
(4)
Verified
Lift Coefficient for a given turn radius
Go
Verified
Turn rate for a high load factor
Go
Verified
Velocity for a given turn rate for a high load factor
Go
Verified
Wing loading for a given turn rate
Go
11 More Flight Envelope Calculators
Go
Flow in open channels
(7)
Verified
Area of flow for a 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 a circular channel considering wetted perimeter
Go
Verified
Wetted perimeter for a circular channel
Go
12 More Flow in open channels Calculators
Go
Flow rate of the electrolyte
(7)
Verified
Atmospheric pressure
Go
Verified
Dynamic viscosity of electrolyte
Go
Verified
Flow rate of the electrolyte
Go
Verified
Gap spacing
Go
Verified
Pressure in flushing hole flow rate electrolyte
Go
Verified
Radius of flushing hole
Go
Verified
Radius of the electrode
Go
Flow through pipes
(2)
Verified
Loss of head due to sudden contraction
Go
Verified
Velocity at section 2-2 for sudden contraction
Go
37 More Flow through pipes Calculators
Go
For Metric Threads
(7)
Verified
Diameter of the 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 the thread from three wire system method
Go
Verified
Pitch of thread when ideal wire diameter is known
Go
Verified
Thread angle when ideal wire diameter is known
Go
Forces on sub-merged bodies
(5)
Verified
Angle of attack for lift coefficient on the airfoil
Go
Verified
Circulation in the location of stagnation points
Go
Verified
Coefficient of lift for an airfoil
Go
Verified
Location of stagnation points for a rotating cylinder in a uniform flow field
Go
Verified
Radius of the cylinder for location of stagnation points
Go
26 More Forces on sub-merged bodies Calculators
Go
Geometry of Turning Process
(6)
Created
Back rake angle for orthogonal cutting
Go
Created
Cutting Speed
Go
Created
Initial diameter of the job
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
3 More Gliding Flight Calculators
Go
Hypersonic Equivalence Principle and Blast-Wave Theory
(5)
Verified
Blunt-nosed flat plate pressure ratio (first approximation)
Go
Verified
formula For creation pressure for the planar blast wave
Go
Verified
Modified Radial coordinate equation for cylindrical blast wave
Go
Verified
Radial coordinate for the planar blast wave,
Go
Verified
Radial coordinate of cylindrical blast wave
Go
11 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators
Go
Hypersonic Flight Paths: Velocity-Altitude Map
(2)
Verified
Radius of curvature for the cylinder-wedge
Go
Verified
Radius of curvature for the sphere-cone body shape
Go
7 More Hypersonic Flight Paths: Velocity-Altitude Map Calculators
Go
Hypersonic Inviscid Flowfields: Approximate Methods
(3)
Verified
Non dimensional radius for hypersonic vehicles
Go
Verified
Transformed conical variable
Go
Verified
Transformed conical variable with wave angle
Go
8 More Hypersonic Inviscid Flowfields: Approximate Methods Calculators
Go
Hypersonic Inviscid Flowfields: Exact Methods
(4)
Verified
Density before the shock formation for expansion wave
Go
Verified
New pressure after the shock formation for compression wave
Go
Verified
Ratio of new and old temperature for expansion waves
Go
Verified
Temperature ratio for unsteady expansion wave
Go
14 More Hypersonic Inviscid Flowfields: Exact Methods Calculators
Go
Hypersonic Small-Disturbance Equations
(2)
Verified
Doty and Rasmussen - normal-force coefficient
Go
Verified
Rasmussen closed-form expression for the shock-wave angle
Go
15 More Hypersonic Small-Disturbance Equations Calculators
Go
Hypersonic Viscous Interactions
(8)
Verified
Mach number over a flat plate using static temperature and wall temperature
Go
Verified
Static temperature of fluid over the flat plate
Go
Verified
Static temperature of the plate using the wall viscosity
Go
Verified
Static temperature over a flat plate under viscous, very high Mach flow
Go
Verified
Total temperature over a flat plate under viscous Mach flow
Go
Verified
Total temperature over a flat plate under viscous very high Mach flow
Go
Verified
Wall temperature of fluid over the flat plate
Go
Verified
Wall temperature of the plate using the wall viscosity
Go
10 More Hypersonic Viscous Interactions Calculators
Go
Ideal flow or Potential flow
(5)
Verified
Dimensions of Rankine half-body
Go
Verified
Distance between source or sink from origin
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
10 More Ideal flow or Potential flow Calculators
Go
Kinematics of flow
(4)
Verified
Angular velocity considering the depth of parabola
Go
Verified
Depth of parabola formed at the free surface of water
Go
Verified
Rate of flow or discharge
Go
Verified
Resultant velocity for two velocity components
Go
3 More Kinematics of flow Calculators
Go
Kirchhoff's law
(6)
Created
Absorptivity of a small body in terms of absorbed radiation and temperature
Go
Created
Emissivity of a small body in terms of emitted radiation and temperature
Go
Created
Radiation absorbed by the small body per unit of its surface area
Go
Created
Radiation emitted by a small body
Go
Created
Temperature of a small body in terms of absorptivity and absorbed radiation
Go
Created
Temperature of a small body in terms of emissivity and emitted radiation
Go
Landing Performance
(1)
Verified
Touchdown velocity for given stall velocity
Go
4 More Landing Performance Calculators
Go
Lowenherz 53
(4)
Verified
Diameter of the measuring wires
Go
Verified
Micrometer measurement/reading lowenherz
Go
Verified
Pitch diameter lowenherz
Go
Verified
pitch of screw lowenherz
Go
Maneuvering Flight
(4)
Verified
Load factor for a given pull-down maneuver rate
Go
Verified
Load factor for a given pull-up maneuver radius
Go
Verified
Pull-down maneuver rate
Go
Verified
Pull-up maneuver radius
Go
8 More Maneuvering Flight Calculators
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
Merchant Force Circle (Mechanics of Orthogonal metal cutting)
(3)
Created
Force normal to shear for given mean shear stress, width of cut, uncut chip thickness & shear angle
Go
Created
Force normal to shear force for given mean normal shear stress & area of shear plane
Go
Created
Mean normal stress in shear plane for given normal force & shear area
Go
35 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
Go
Metal Cutting and 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
4 More Metal Cutting and tools Calculators
Go
Metrology
(1)
Verified
Tolerance unit (i)
Go
Modern design-oriented code
(1)
Verified
Convective heat transfer to the surface
Go
1 More Modern design-oriented code Calculators
Go
Molar diffusion
(2)
Verified
Steady state equimolal counter diffusion between gases (mass flux)
Go
Verified
Steady state equimolal counter diffusion of component A into B ( mass flux)
Go
15 More Molar diffusion Calculators
Go
Net force acting on the electrode
(3)
Verified
Ambient atmospheric pressure
Go
Verified
Net force acting on the electrode
Go
Verified
Pressure in flushing hole net force electrode
Go
Newtonian Flow
(5)
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
Verified
Pressure coefficient for slender bodies of revolution
Go
9 More Newtonian Flow Calculators
Go
Normal Shock Waves
(5)
Verified
Characteristic Mach Number behind shock
Go
Verified
Entropy change across normal shock
Go
Verified
Relation between Characteristic Mach number and Mach number
Go
Verified
Shock strength
Go
Verified
Velocity behind a normal shock
Go
24 More Normal Shock Waves Calculators
Go
Notches and Weirs
(8)
Verified
Discharge over a broad-crested weir for head of liquid at middle
Go
Verified
Discharge over a broad-crested weir with velocity approach
Go
Verified
Discharge over a trapezoidal notch or weir
Go
Verified
Discharge over a triangular notch or weir
Go
Verified
Head of liquid above the V-notch
Go
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 approach
Go
Verified
Time required to empty a tank with a triangular weir or notch
Go
19 More Notches and Weirs Calculators
Go
Oblique Shock and Expansion Waves
(2)
Verified
Component of Downstream Mach normal to oblique shock
Go
Verified
Flow deflection angle
Go
17 More Oblique Shock and Expansion Waves Calculators
Go
Orifices and Mouthpieces
(10)
Verified
Absolute pressure head at constant head and atmospheric pressure head
Go
Verified
Area of tank while considering time for emptying a tank
Go
Verified
Atmospheric pressure head at constant head and absolute pressure head
Go
Verified
Co-efficient of discharge
Go
Verified
Co-efficient of discharge considering time for emptying a tank
Go
Verified
Co-efficient of discharge for area and velocity
Go
Verified
Co-efficient of velocity for horizontal and vertical distance
Go
Verified
Loss of head due to sudden enlargement
Go
Verified
Time of emptying a tank through an orifice at bottom
Go
Verified
Velocity of liquid at C-C for Hc, Ha, and H
Go
23 More Orifices and Mouthpieces 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 a pipe in square section
Go
Created
Inner surface temperature of a pipe with eccentric lagging
Go
Created
Length of a pipe with eccentric lagging
Go
Created
outer surface temperature of a pipe in square section
Go
Created
outer surface temperature of a pipe with eccentric lagging
Go
Created
Thermal conductivity for a pipe with eccentric lagging
Go
Created
Thermal resistance for a pipe in square section
Go
Created
Thermal resistance of a pipe with eccentric lagging
Go
Plane walls
(22)
Created
Area of a composite wall of 2 layers
Go
Created
Area of a composite wall of 3 layers
Go
Created
Area of the plane wall required for a given temperature difference
Go
Created
Heat flow rate through a composite wall of 2 layers in series
Go
Created
Heat flow rate through a composite wall of 3 layers in series
Go
Created
Inner surface temperature of a composite wall of 2 layers in series
Go
Created
Inner surface temperature of a composite wall of 3 layers in series
Go
Created
Inner surface temperature of a plane wall
Go
Created
Interface temperature of composite wall of 2 layers when inner surface temperature is known
Go
Created
Interface temperature of composite wall of 2 layers when outer surface temperature is known
Go
Created
Length of the 2nd layer of the composite wall for a given temperature difference
Go
Created
Length of the 3rd layer of the composite wall for a given temperature difference
Go
Created
Outer surface temperature of a composite wall of 2 layers for a given heat flow rate
Go
Created
Outer surface temperature of a composite wall of 3 layers for a given heat flow rate
Go
Created
Outer surface temperature of the wall for a given heat flow rate
Go
Created
Temperature at distance x from the inner surface in the wall
Go
Created
Thermal conductivity of the material required to maintain a given temperature difference
Go
Created
Thermal resistance of a composite wall with 2 layers in series
Go
Created
Thermal resistance of a composite wall with 3 layers in series
Go
Created
Thermal Resistance of a wall
Go
Created
Thickness of the plane wall required for a given temperature difference
Go
Created
Total thermal resistance of a plain wall with convection on either side
Go
Polymer Matrix Composites (PMC)
(1)
Verified
Elastic modulus of the composite in the transverse direction
Go
17 More Polymer Matrix Composites (PMC) Calculators
Go
Possible surface defects in EDM
(5)
Verified
Overcut constant A
Go
Verified
Overcut constant B
Go
Verified
Overcut produced per side
Go
Verified
Taper produced due to side sparks
Go
Verified
Upper diameter of hole
Go
10 More Possible surface defects in EDM Calculators
Go
Power Required for Level Unaccelerated Flight
(4)
Verified
Coefficient of Drag due to lift for minimum power required
Go
Verified
Freestream velocity for given required power
Go
Verified
Freestream Velocity for given total drag
Go
Verified
Zero-lift drag coefficient for minimum power required
Go
6 More Power Required for Level Unaccelerated Flight Calculators
Go
Pressure distribution in the flushing gap
(6)
Verified
Atmospheric pressure at electrode tip
Go
Verified
Pressure distribution in the flushing gap
Go
Verified
Pressure in flushing hole
Go
Verified
Radial location of pressure distribution
Go
Verified
Radius of flushing hole EDM
Go
Verified
Radius of the electrode from pressure flushing hole
Go
Radiation
(7)
Created
Radiation energy emitted by a black body in given time interval when emissive power is known
Go
Created
Radiation energy emitted by a black body in given time interval when temperature is known
Go
Created
Radiation energy emitted by a black body per unit time and surface area
Go
Created
Spectral black body emissive power (Planck's law)
Go
Created
Surface area of the black body required to emit certain amount of radiation energy
Go
Created
Temperature of the black body to emit a certain amount of radiation energy
Go
Created
Time required to emit a specified amount of radiation energy from the black body
Go
Range and Endurance of Jet Airplane
(2)
Verified
Endurance of Jet Airplane
Go
Verified
Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane
Go
5 More Range and Endurance of Jet Airplane Calculators
Go
Rate of Climb
(3)
Verified
Excess power for given rate of climb
Go
Verified
Velocity of aircraft at a given rate of climb
Go
Verified
Velocity of aircraft for given excess power
Go
7 More Rate of Climb Calculators
Go
Reference Temperature Method
(3)
Verified
Reynolds number for chord length
Go
Verified
Static density of the plate using chord length for flat plate case
Go
Verified
Static velocity of the plate using chord length for flat plate case
Go
12 More Reference Temperature Method Calculators
Go
Sharp V
(4)
Verified
Diameter of the wire used Sharp V
Go
Verified
Micrometer measurement/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
Spheres
(11)
Created
Convection resistance for a spherical layer
Go
Created
Heat flow rate through a spherical composite wall of 2 layers in series
Go
Created
Heat flow rate through a spherical wall
Go
Created
Inner surface temperature of a spherical wall
Go
Created
Outer surface temperature of a spherical wall
Go
Created
Thermal resistance of a spherical composite wall of 2 layers in series with convection
Go
Created
Thermal resistance of a spherical wall
Go
Created
Thickness of the spherical wall to maintain given temperature difference
Go
Created
Total thermal resistance of a spherical wall of 2 layers without convection
Go
Created
Total thermal resistance of a spherical wall of 3 layers without convection
Go
Created
Total thermal resistance of a spherical wall with convection on either side
Go
Tail Contribution
(1)
Verified
Angle of attack of the wing
Go
20 More Tail Contribution Calculators
Go
Takeoff Performance
(2)
Verified
Maximum Lift coefficient for given stall velocity
Go
Verified
Stall velocity for given liftoff velocity
Go
12 More Takeoff Performance Calculators
Go
The 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
1 More The Drag Polar Calculators
Go
Thread measurement
(4)
Verified
Diameter of the wire used in measurement over wires method
Go
Verified
Micrometer reading from measurement over wires method
Go
Verified
Pitch diameter from measurement over wires method
Go
Verified
Pitch of the thread from measurement over wires method
Go
Thrust Required for Level Unaccelerated Flight
(5)
Verified
Coefficient of Lift for given thrust-to-weight ratio
Go
Verified
Lift for a level, unaccelerated flight at negligible thrust angle
Go
Verified
Minimum Thrust required
Go
Verified
Thrust required for level, unaccelerated flight
Go
Verified
Weight of aircraft for a level, unaccelerated flight at negligible thrust angle
Go
7 More Thrust Required for Level Unaccelerated Flight Calculators
Go
Tool Life And Tool Wear
(1)
Verified
Tool temperature
Go
15 More Tool Life And Tool Wear Calculators
Go
Turning Flight
(4)
Verified
Lift during level turn
Go
Verified
Lift for a given load factor
Go
Verified
Load factor for a given turn rate
Go
Verified
Turn radius
Go
8 More Turning Flight Calculators
Go
Unsymmetrical threads
(6)
Verified
Best size wire
Go
Verified
Best wire size for modified buttress 45deg and 7deg
Go
Verified
Micrometer reading/measurement
Go
Verified
Pitch diameter unsymmetrical threads
Go
Verified
Pitch for modified buttress 45deg and 7deg
Go
Verified
Pitch of screw unsymmetrical threads
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Viscous flow
(16)
Verified
Diameter of shaft for speed and shear stress of fluid in journal bearing
Go
Verified
Difference of pressure for viscous or laminar flow
Go
Verified
External or outer radius of collar for total torque
Go
Verified
Internal or inner radius of collar for total torque
Go
Verified
Power absorbed in collar bearing
Go
Verified
Power absorbed in foot-step bearing
Go
Verified
Radius of shaft for torque required in foot-step bearing
Go
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
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
Verified
Torque required to overcome viscous resistance in collar bearing
Go
Verified
Torque required to overcome viscous resistance in foot-step bearing
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36 More Viscous flow Calculators
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Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating
(4)
Verified
internal energy for hypersonic flow
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Verified
Non dimensional internal energy parameter
Go
Verified
Static enthalpy
Go
Verified
Wall temperature calculator due to internal energy
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12 More Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating 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
Go
Verified
Wear Ratio
Go
Whitworth 55deg. included angle
(4)
Verified
Diameter of the wire used
Go
Verified
Micrometer reading/measurement whitworth
Go
Verified
Pitch diameter whitworth
Go
Verified
pitch of screw threads whitworth
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