Recovery Factor using Temperature Solution

STEP 0: Pre-Calculation Summary
Formula Used
Recovery Factor = (Adiabatic Wall Temperature-Static Temperature)/(Total Temperature-Static Temperature)
r = (Twall-Tstatic)/(Tt-Tstatic)
This formula uses 4 Variables
Variables Used
Recovery Factor - The Recovery Factor is a measure of the efficiency of fluid recovery in viscous flow scenarios, indicating how much of the fluid's energy is successfully harnessed.
Adiabatic Wall Temperature - (Measured in Kelvin) - The Adiabatic Wall Temperature is the temperature of a wall in a fluid flow scenario, assuming no heat transfer occurs between the wall and the fluid.
Static Temperature - (Measured in Kelvin) - The Static Temperature is the temperature of a fluid at rest, providing essential information about its thermal state in viscous flow scenarios.
Total Temperature - (Measured in Kelvin) - The Total Temperature is the temperature of a fluid that accounts for both its thermal energy and the kinetic energy due to its motion.
STEP 1: Convert Input(s) to Base Unit
Adiabatic Wall Temperature: 425 Kelvin --> 425 Kelvin No Conversion Required
Static Temperature: 350 Kelvin --> 350 Kelvin No Conversion Required
Total Temperature: 377.7777 Kelvin --> 377.7777 Kelvin No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
r = (Twall-Tstatic)/(Tt-Tstatic) --> (425-350)/(377.7777-350)
Evaluating ... ...
r = 2.70000756002117
STEP 3: Convert Result to Output's Unit
2.70000756002117 --> No Conversion Required
FINAL ANSWER
2.70000756002117 2.700008 <-- Recovery Factor
(Calculation completed in 00.004 seconds)

Credits

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Amrita School of Engineering (ASE), Vallikavu
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Viscous Flow Calculators

Aerodynamic Heating Equation for Stanton number
​ LaTeX ​ Go Stanton Number = Local Heat Transfer Rate/(Static Density*Static Velocity*(Adiabatic Wall Enthalpy-Wall Enthalpy))
Adiabatic Wall Enthalpy for Flat Plate
​ LaTeX ​ Go Adiabatic Wall Enthalpy = Static Enthalpy+Recovery Factor*(Total Specific Enthalpy-Static Enthalpy)
Adiabatic Wall Enthalpy using Recovery Factor
​ LaTeX ​ Go Adiabatic Wall Enthalpy = Static Enthalpy+Recovery Factor*(Static Velocity^2)/2
Coefficient of Friction using Stanton Number for Flat Plate Case
​ LaTeX ​ Go Coefficient of Friction = (2*Stanton Number)/(Prandtl Number^(-2/3))

Recovery Factor using Temperature Formula

​LaTeX ​Go
Recovery Factor = (Adiabatic Wall Temperature-Static Temperature)/(Total Temperature-Static Temperature)
r = (Twall-Tstatic)/(Tt-Tstatic)

What is Enthalpy?

Enthalpy is a property of a thermodynamic system, defined as the sum of the system's internal energy and the product of its pressure and volume.

How to Calculate Recovery Factor using Temperature?

Recovery Factor using Temperature calculator uses Recovery Factor = (Adiabatic Wall Temperature-Static Temperature)/(Total Temperature-Static Temperature) to calculate the Recovery Factor, Recovery Factor using Temperature formula is defined as a dimensionless quantity that characterizes the heat transfer between a flat plate and a fluid in viscous flow, providing a measure of the temperature difference between the wall and the static fluid. Recovery Factor is denoted by r symbol.

How to calculate Recovery Factor using Temperature using this online calculator? To use this online calculator for Recovery Factor using Temperature, enter Adiabatic Wall Temperature (Twall), Static Temperature (Tstatic) & Total Temperature (Tt) and hit the calculate button. Here is how the Recovery Factor using Temperature calculation can be explained with given input values -> 3 = (425-350)/(377.7777-350).

FAQ

What is Recovery Factor using Temperature?
Recovery Factor using Temperature formula is defined as a dimensionless quantity that characterizes the heat transfer between a flat plate and a fluid in viscous flow, providing a measure of the temperature difference between the wall and the static fluid and is represented as r = (Twall-Tstatic)/(Tt-Tstatic) or Recovery Factor = (Adiabatic Wall Temperature-Static Temperature)/(Total Temperature-Static Temperature). The Adiabatic Wall Temperature is the temperature of a wall in a fluid flow scenario, assuming no heat transfer occurs between the wall and the fluid, The Static Temperature is the temperature of a fluid at rest, providing essential information about its thermal state in viscous flow scenarios & The Total Temperature is the temperature of a fluid that accounts for both its thermal energy and the kinetic energy due to its motion.
How to calculate Recovery Factor using Temperature?
Recovery Factor using Temperature formula is defined as a dimensionless quantity that characterizes the heat transfer between a flat plate and a fluid in viscous flow, providing a measure of the temperature difference between the wall and the static fluid is calculated using Recovery Factor = (Adiabatic Wall Temperature-Static Temperature)/(Total Temperature-Static Temperature). To calculate Recovery Factor using Temperature, you need Adiabatic Wall Temperature (Twall), Static Temperature (Tstatic) & Total Temperature (Tt). With our tool, you need to enter the respective value for Adiabatic Wall Temperature, Static Temperature & Total Temperature 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 Recovery Factor?
In this formula, Recovery Factor uses Adiabatic Wall Temperature, Static Temperature & Total Temperature. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Recovery Factor = sqrt(Prandtl Number)
  • Recovery Factor = (Adiabatic Wall Enthalpy-Static Enthalpy)/(Total Specific Enthalpy-Static Enthalpy)
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