Specific Heat at Constant Pressure for Transient Flow Calculator

✖The Transient Prandtl Number is a dimensionless quantity that characterizes the relationship between thermal and momentum diffusivity in transient heat transfer during hypersonic flow.ⓘ Transient Prandtl Number [Pr_T]			+10% -10%
✖The Transition Thermal Conductivity is the measure of heat transfer through a material during the transition phase in hypersonic flow over a flat plate.ⓘ Transition Thermal Conductivity [k_T]			+10% -10%
✖The Eddy Viscosity is a measure of the turbulent momentum transfer in a fluid, influencing the flow characteristics around surfaces in hypersonic conditions.ⓘ Eddy Viscosity [μ_T]			+10% -10%

✖The Molar Specific Heat Capacity at Constant Pressure is the amount of heat required to raise the temperature of one mole of a substance at constant pressure.ⓘ Specific Heat at Constant Pressure for Transient Flow [C_{p molar}]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Hypersonic Flow Formula PDF PDF Image

Specific Heat at Constant Pressure for Transient Flow Solution

STEP 0: Pre-Calculation Summary

Formula Used

Molar Specific Heat Capacity at Constant Pressure = (Transient Prandtl Number*Transition Thermal Conductivity)/Eddy Viscosity
C_{p molar} = (Pr_T*k_T)/μ_T
This formula uses 4 Variables

Variables Used

Molar Specific Heat Capacity at Constant Pressure - (Measured in Joule Per Kelvin Per Mole) - The Molar Specific Heat Capacity at Constant Pressure is the amount of heat required to raise the temperature of one mole of a substance at constant pressure.
Transient Prandtl Number - The Transient Prandtl Number is a dimensionless quantity that characterizes the relationship between thermal and momentum diffusivity in transient heat transfer during hypersonic flow.
Transition Thermal Conductivity - (Measured in Watt per Meter per K) - The Transition Thermal Conductivity is the measure of heat transfer through a material during the transition phase in hypersonic flow over a flat plate.
Eddy Viscosity - (Measured in Pascal Second) - The Eddy Viscosity is a measure of the turbulent momentum transfer in a fluid, influencing the flow characteristics around surfaces in hypersonic conditions.

STEP 1: Convert Input(s) to Base Unit

Transient Prandtl Number: 2.4 --> No Conversion Required
Transition Thermal Conductivity: 112 Watt per Meter per K --> 112 Watt per Meter per K No Conversion Required
Eddy Viscosity: 22.03279 Poise --> 2.203279 Pascal Second (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_{p molar} = (Pr_T*k_T)/μ_T --> (2.4*112)/2.203279

Evaluating ... ...

C_{p molar} = 121.999982752979

STEP 3: Convert Result to Output's Unit

121.999982752979 Joule Per Kelvin Per Mole --> No Conversion Required

FINAL ANSWER

121.999982752979 ≈ 122 Joule Per Kelvin Per Mole <-- Molar Specific Heat Capacity at Constant Pressure

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Flat Plate for Viscous Flow Case » Hypersonic Transition » Specific Heat at Constant Pressure for Transient Flow

Credits

Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ more calculators!

< Hypersonic Transition Calculators

Static Velocity at Transition Point

LaTeX Go Static Velocity = (Transition Reynolds Number*Static Viscosity)/(Static Density*Location Transition Point)

Static Density at Transition Point

LaTeX Go Static Density = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Location Transition Point)

Location of Transition Point

LaTeX Go Location Transition Point = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)

Transition Reynolds Number

LaTeX Go Transition Reynolds Number = (Static Density*Static Velocity*Location Transition Point)/Static Viscosity

Specific Heat at Constant Pressure for Transient Flow Formula

LaTeX Go

Molar Specific Heat Capacity at Constant Pressure = (Transient Prandtl Number*Transition Thermal Conductivity)/Eddy Viscosity
C_{p molar} = (Pr_T*k_T)/μ_T

What is Prandtl Number?

The Prandtl Number is a dimensionless number approximating the ratio of momentum diffusivity to thermal diffusivity. The Prandtl Number is often used in heat transfer and free and forced convection calculations. It depends on the fluid properties.

How to Calculate Specific Heat at Constant Pressure for Transient Flow?

Specific Heat at Constant Pressure for Transient Flow calculator uses Molar Specific Heat Capacity at Constant Pressure = (Transient Prandtl Number*Transition Thermal Conductivity)/Eddy Viscosity to calculate the Molar Specific Heat Capacity at Constant Pressure, Specific Heat at Constant Pressure for Transient Flow formula is defined as the heat capacity of a substance at constant pressure, which is a critical parameter in understanding the thermodynamic behavior of fluids in transient flow conditions, particularly in flat plate viscous flow cases. Molar Specific Heat Capacity at Constant Pressure is denoted by C_{p molar} symbol.

How to calculate Specific Heat at Constant Pressure for Transient Flow using this online calculator? To use this online calculator for Specific Heat at Constant Pressure for Transient Flow, enter Transient Prandtl Number (Pr_T), Transition Thermal Conductivity (k_T) & Eddy Viscosity (μ_T) and hit the calculate button. Here is how the Specific Heat at Constant Pressure for Transient Flow calculation can be explained with given input values -> 134.4 = (2.4*112)/2.203279.

FAQ

What is Specific Heat at Constant Pressure for Transient Flow?

Specific Heat at Constant Pressure for Transient Flow formula is defined as the heat capacity of a substance at constant pressure, which is a critical parameter in understanding the thermodynamic behavior of fluids in transient flow conditions, particularly in flat plate viscous flow cases and is represented as C_{p molar} = (Pr_T*k_T)/μ_T or Molar Specific Heat Capacity at Constant Pressure = (Transient Prandtl Number*Transition Thermal Conductivity)/Eddy Viscosity. The Transient Prandtl Number is a dimensionless quantity that characterizes the relationship between thermal and momentum diffusivity in transient heat transfer during hypersonic flow, The Transition Thermal Conductivity is the measure of heat transfer through a material during the transition phase in hypersonic flow over a flat plate & The Eddy Viscosity is a measure of the turbulent momentum transfer in a fluid, influencing the flow characteristics around surfaces in hypersonic conditions.

How to calculate Specific Heat at Constant Pressure for Transient Flow?

Specific Heat at Constant Pressure for Transient Flow formula is defined as the heat capacity of a substance at constant pressure, which is a critical parameter in understanding the thermodynamic behavior of fluids in transient flow conditions, particularly in flat plate viscous flow cases is calculated using Molar Specific Heat Capacity at Constant Pressure = (Transient Prandtl Number*Transition Thermal Conductivity)/Eddy Viscosity. To calculate Specific Heat at Constant Pressure for Transient Flow, you need Transient Prandtl Number (Pr_T), Transition Thermal Conductivity (k_T) & Eddy Viscosity (μ_T). With our tool, you need to enter the respective value for Transient Prandtl Number, Transition Thermal Conductivity & Eddy Viscosity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

Home

FREE PDFs

🔍 Search