Large Mach Number over Flat Plate using Static Temperature and Wall Temperature Calculator

✖Wall Temperature is the temperature at the wall.ⓘ Wall Temperature [Tw]			+10% -10%
✖The Static Temperature is defined as the temperature of the gas if it had no ordered motion and was not flowing.ⓘ Static Temperature [T_static]			+10% -10%
✖The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.ⓘ Specific Heat Ratio [γ]			+10% -10%

✖Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.ⓘ Large Mach Number over Flat Plate using Static Temperature and Wall Temperature [M]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Hypersonic Flow Formula PDF PDF Image

Large Mach Number over Flat Plate using Static Temperature and Wall Temperature Solution

STEP 0: Pre-Calculation Summary

Formula Used

Mach Number = sqrt((Wall Temperature/Static Temperature)/((Specific Heat Ratio-1)/2))
M = sqrt((Tw/T_static)/((γ-1)/2))
This formula uses 1 Functions, 4 Variables

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Mach Number - Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Wall Temperature - (Measured in Kelvin) - Wall Temperature is the temperature at the wall.
Static Temperature - (Measured in Kelvin) - The Static Temperature is defined as the temperature of the gas if it had no ordered motion and was not flowing.
Specific Heat Ratio - The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.

STEP 1: Convert Input(s) to Base Unit

Wall Temperature: 15 Kelvin --> 15 Kelvin No Conversion Required
Static Temperature: 350 Kelvin --> 350 Kelvin No Conversion Required
Specific Heat Ratio: 1.6 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

M = sqrt((Tw/T_static)/((γ-1)/2)) --> sqrt((15/350)/((1.6-1)/2))

Evaluating ... ...

M = 0.377964473009227

STEP 3: Convert Result to Output's Unit

0.377964473009227 --> No Conversion Required

FINAL ANSWER

0.377964473009227 ≈ 0.377964 <-- Mach Number

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Hypersonic Viscous Interactions » Supersonic Aerothermodynamics » Large Mach Number over Flat Plate using Static Temperature and Wall Temperature

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!

< Supersonic Aerothermodynamics Calculators

Mach Number over Flat Plate using Static Temperature and Wall Temperature

LaTeX Go Mach Number = sqrt((Temperature of Wall in Kelvin/Static Temperature-1)/((Specific Heat Ratio-1)/2))

Total Temperature over Flat Plate under Viscous Mach Flow

LaTeX Go Total Temperature = Static Temperature+Static Temperature*((Specific Heat Ratio-1)/2)*Mach Number^2

Viscosity of Wall using Wall Temperature and Static Temperature

LaTeX Go Wall Viscosity = Static Viscosity*Wall Temperature/Static Temperature

Wall Density of Fluid over Flat Plate

LaTeX Go Wall Density = Static Density/(Wall Temperature/Static Temperature)

Large Mach Number over Flat Plate using Static Temperature and Wall Temperature Formula

LaTeX Go

Mach Number = sqrt((Wall Temperature/Static Temperature)/((Specific Heat Ratio-1)/2))
M = sqrt((Tw/T_static)/((γ-1)/2))

What is Mach number?

Mach number is a dimensionless quantity in fluid dynamics representing the ratio of flow velocity past a boundary to the local speed of sound.

How to Calculate Large Mach Number over Flat Plate using Static Temperature and Wall Temperature?

Large Mach Number over Flat Plate using Static Temperature and Wall Temperature calculator uses Mach Number = sqrt((Wall Temperature/Static Temperature)/((Specific Heat Ratio-1)/2)) to calculate the Mach Number, The Large Mach number over flat plate using static temperature and wall temperature formula is defined as the function of specific heat ratio, wall temperature, and static temperature of the flow. Mach Number is denoted by M symbol.

How to calculate Large Mach Number over Flat Plate using Static Temperature and Wall Temperature using this online calculator? To use this online calculator for Large Mach Number over Flat Plate using Static Temperature and Wall Temperature, enter Wall Temperature (Tw), Static Temperature (T_static) & Specific Heat Ratio (γ) and hit the calculate button. Here is how the Large Mach Number over Flat Plate using Static Temperature and Wall Temperature calculation can be explained with given input values -> 0.377964 = sqrt((15/350)/((1.6-1)/2)).

FAQ

What is Large Mach Number over Flat Plate using Static Temperature and Wall Temperature?

The Large Mach number over flat plate using static temperature and wall temperature formula is defined as the function of specific heat ratio, wall temperature, and static temperature of the flow and is represented as M = sqrt((Tw/T_static)/((γ-1)/2)) or Mach Number = sqrt((Wall Temperature/Static Temperature)/((Specific Heat Ratio-1)/2)). Wall Temperature is the temperature at the wall, The Static Temperature is defined as the temperature of the gas if it had no ordered motion and was not flowing & The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.

How to calculate Large Mach Number over Flat Plate using Static Temperature and Wall Temperature?

The Large Mach number over flat plate using static temperature and wall temperature formula is defined as the function of specific heat ratio, wall temperature, and static temperature of the flow is calculated using Mach Number = sqrt((Wall Temperature/Static Temperature)/((Specific Heat Ratio-1)/2)). To calculate Large Mach Number over Flat Plate using Static Temperature and Wall Temperature, you need Wall Temperature (Tw), Static Temperature (T_static) & Specific Heat Ratio (γ). With our tool, you need to enter the respective value for Wall Temperature, Static Temperature & Specific Heat Ratio 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 Mach Number?

In this formula, Mach Number uses Wall Temperature, Static Temperature & Specific Heat Ratio. We can use 1 other way(s) to calculate the same, which is/are as follows -

Mach Number = sqrt((Temperature of Wall in Kelvin/Static Temperature-1)/((Specific Heat Ratio-1)/2))

Home

FREE PDFs

🔍 Search