Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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11 Other formulas that you can solve using the same Inputs

Nusselt number for hypersonic vehicle
Nusselt Number=((Local heat transfer rate*Distance from the nose tip to required base dia))/(Thermal Conductivity*(Adiabatic wall temperature-Wall temperature)) GO
Thermal conductivity at the edge of the boundary layer equation using Nusselt's number
Thermal Conductivity=(Local heat transfer rate*Distance from the nose tip to required base dia)/(Nusselt Number*(Adiabatic wall temperature-Wall temperature)) GO
Aerodynamic heating to the surface
Local heat transfer rate=Static density*Static velocity*Stanton Number*(Adiabatic wall enthalpy-Wall enthalpy) GO
Static viscosity calculation using Chapman–Rubesin factor
static viscosity=(Density*Kinematic viscosity )/(Chapman–Rubesin factor*Static density) GO
Static velocity equation using skin friction coefficient
Static velocity=sqrt((2*Shear Stress)/(Local skin-friction coefficient*Static density)) GO
Chapman–Rubesin factor
Chapman–Rubesin factor=(Density*Kinematic viscosity )/(Static density*static viscosity) GO
local shear stress at the wall
Shear Stress=(0.5)*Local skin-friction coefficient*Static density*(static viscosity^2) GO
Static Density equation using skin friction coefficient
Static density=(2*Shear Stress)/(Local skin-friction coefficient*(Static velocity^2)) GO
Viscosity calculation using Chapman–Rubesin factor
Kinematic viscosity =Chapman–Rubesin factor*Static density*static viscosity/(Density) GO
Density calculation using Chapman–Rubesin factor
Density=Chapman–Rubesin factor*Static density*static viscosity/(Kinematic viscosity ) GO
Local skin-friction coefficient
Local skin-friction coefficient=(2*Shear Stress)/(Static density*(Static velocity^2)) GO

3 Other formulas that calculate the same Output

Adiabatic wall enthalpy over flat plate using Stanton number
Adiabatic wall enthalpy=(Local heat transfer rate/(Freestream density*Freestream Velocity*Stanton Number))+Wall enthalpy GO
Adiabatic wall enthalpy for flat plate
Adiabatic wall enthalpy=Static enthalpy+Recovery factor*(Total Specific enthalpy-Static enthalpy) GO
Adiabatic wall enthalpy using recovery factor
Adiabatic wall enthalpy=Static enthalpy+Recovery factor*(Static velocity^2)/2 GO

Adiabatic wall enthalpy using Stanton number Formula

Adiabatic wall enthalpy=Local heat transfer rate/(Static density*Static velocity*Stanton Number)+Wall enthalpy
h<sub>aw</sub>=q<sub>w</sub>/(ρ<sub>e</sub>*u<sub>e</sub>*C<sub>H</sub>)+h<sub>w</sub>
More formulas
Local skin-friction coefficient GO
local shear stress at the wall GO
Static Density equation using skin friction coefficient GO
Static velocity equation using skin friction coefficient GO
Nusselt number for hypersonic vehicle GO
local heat-transfer rate using Nusselt's number GO
Thermal conductivity at the edge of the boundary layer equation using Nusselt's number GO
Stanton number for hypersonic vehicle GO
Local heat-transfer rate calculation using Stanton number GO
Static density equation using Stanton number GO
Static velocity using Stanton number GO
Enthalpy of wall using Stanton number GO
Nusselt's number with Reynolds number, the Stanton number and Prandtl number GO
Reynolds number for given Nusselt's number, Stanton number and Prandtl number GO
Stanton number with Reynolds number, Nusselt's number, Stanton number and Prandtl number GO
Prandtl number with Reynolds number, Nusselt's number, Stanton number and Stanton number GO
Skin friction coefficient for incompressible flow GO
viscosity around the wall GO
Static viscosity relation using temperature of wall GO

What is Stanton number?

The Stanton number, St, is a dimensionless number that measures the ratio of heat transferred into a fluid to the thermal capacity of fluid

How to Calculate Adiabatic wall enthalpy using Stanton number?

Adiabatic wall enthalpy using Stanton number calculator uses Adiabatic wall enthalpy=Local heat transfer rate/(Static density*Static velocity*Stanton Number)+Wall enthalpy to calculate the Adiabatic wall enthalpy, Adiabatic wall enthalpy using Stanton number formula is defined as the interrelation of local heat transfer, static density and velocity of the fluid, adiabatic and wall enthalpy and wall enthalpy. Adiabatic wall enthalpy and is denoted by haw symbol.

How to calculate Adiabatic wall enthalpy using Stanton number using this online calculator? To use this online calculator for Adiabatic wall enthalpy using Stanton number, enter Local heat transfer rate (qw), Static density e), Static velocity (ue), Stanton Number (CH) and Wall enthalpy (hw) and hit the calculate button. Here is how the Adiabatic wall enthalpy using Stanton number calculation can be explained with given input values -> 10 = 10/(100000000*10*1)+10.

FAQ

What is Adiabatic wall enthalpy using Stanton number?
Adiabatic wall enthalpy using Stanton number formula is defined as the interrelation of local heat transfer, static density and velocity of the fluid, adiabatic and wall enthalpy and wall enthalpy and is represented as haw=qw/(ρe*ue*CH)+hw or Adiabatic wall enthalpy=Local heat transfer rate/(Static density*Static velocity*Stanton Number)+Wall enthalpy. Local heat transfer rate, is that energy per second per unit area, Static density, is the density of the fluid when its not moving, or the density of fluid if we are moving relative to the fluid, Static velocity is the velocity of fluid at a point in the fluid, or velocity in the continuous flow, The Stanton number is a dimensionless number that measures the ratio of heat transferred into a fluid to the thermal capacity of the fluid and Wall enthalpy is the Enthalpy of a fluid flowing around a solid body; it corresponds to the adiabatic wall temperature.
How to calculate Adiabatic wall enthalpy using Stanton number?
Adiabatic wall enthalpy using Stanton number formula is defined as the interrelation of local heat transfer, static density and velocity of the fluid, adiabatic and wall enthalpy and wall enthalpy is calculated using Adiabatic wall enthalpy=Local heat transfer rate/(Static density*Static velocity*Stanton Number)+Wall enthalpy. To calculate Adiabatic wall enthalpy using Stanton number, you need Local heat transfer rate (qw), Static density e), Static velocity (ue), Stanton Number (CH) and Wall enthalpy (hw). With our tool, you need to enter the respective value for Local heat transfer rate, Static density, Static velocity, Stanton Number and Wall enthalpy and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Adiabatic wall enthalpy?
In this formula, Adiabatic wall enthalpy uses Local heat transfer rate, Static density, Static velocity, Stanton Number and Wall enthalpy. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Adiabatic wall enthalpy=Static enthalpy+Recovery factor*(Static velocity^2)/2
  • Adiabatic wall enthalpy=Static enthalpy+Recovery factor*(Total Specific enthalpy-Static enthalpy)
  • Adiabatic wall enthalpy=(Local heat transfer rate/(Freestream density*Freestream Velocity*Stanton Number))+Wall enthalpy
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