Non-Dimensional Pressure for High Mach Number Calculator

✖Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.ⓘ Wave Angle [β]			+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%

✖Non Dimensionalized Pressure For High Mech Number is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters.ⓘ Non-Dimensional Pressure for High Mach Number [p_mech]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Approximate Methods of Hypersonic Inviscid Flowfields Formulas PDF PDF Image

Non-Dimensional Pressure for High Mach Number Solution

STEP 0: Pre-Calculation Summary

Formula Used

Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1)
p_mech = 2*(sin(β))^2/(γ+1)
This formula uses 1 Functions, 3 Variables

Functions Used

sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)

Variables Used

Non Dimensionalized Pressure For High Mech Number - Non Dimensionalized Pressure For High Mech Number is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters.
Wave Angle - (Measured in Radian) - Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.
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

Wave Angle: 0.286 Radian --> 0.286 Radian No Conversion Required
Specific Heat Ratio: 1.6 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

p_mech = 2*(sin(β))^2/(γ+1) --> 2*(sin(0.286))^2/(1.6+1)

Evaluating ... ...

p_mech = 0.061223066160415

STEP 3: Convert Result to Output's Unit

0.061223066160415 --> No Conversion Required

FINAL ANSWER

0.061223066160415 ≈ 0.061223 <-- Non Dimensionalized Pressure For High Mech Number

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Approximate Methods of Hypersonic Inviscid Flowfields » Non-Dimensional Pressure for High Mach Number

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!

< Approximate Methods of Hypersonic Inviscid Flowfields Calculators

Non-Dimensional Pressure for High Mach Number

LaTeX Go Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1)

Non-Dimensional Pressure

LaTeX Go Non Dimensionalized Pressure = Pressure/(Density*Freestream Velocity^2)

Non-Dimensional Density for High Mach Number

LaTeX Go Non Dimensionalized Density = (Specific Heat Ratio+1)/(Specific Heat Ratio-1)

Non-Dimensional Density

LaTeX Go Non Dimensionalized Density = Density/Liquid Density

Non-Dimensional Pressure for High Mach Number Formula

LaTeX Go

Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1)
p_mech = 2*(sin(β))^2/(γ+1)

What is Non-dimensionalization ?

n fluid mechanics, non-dimensionalization of the Navier–Stokes equations is the conversion of the Navier–Stokes equation to a nondimensional form. This technique can ease the analysis of the problem at hand, and reduce the number of free parameters

How to Calculate Non-Dimensional Pressure for High Mach Number?

Non-Dimensional Pressure for High Mach Number calculator uses Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1) to calculate the Non Dimensionalized Pressure For High Mech Number, Non-Dimensional Pressure for High Mach Number is a dimensionless quantity used in aerodynamics to characterize the pressure distribution on a body moving at high speeds, typically at Mach numbers greater than 0.3. It is defined as the ratio of the actual pressure to the dynamic pressure, and it helps in analyzing compressible flow phenomena. Non Dimensionalized Pressure For High Mech Number is denoted by p_mech symbol.

How to calculate Non-Dimensional Pressure for High Mach Number using this online calculator? To use this online calculator for Non-Dimensional Pressure for High Mach Number, enter Wave Angle (β) & Specific Heat Ratio (γ) and hit the calculate button. Here is how the Non-Dimensional Pressure for High Mach Number calculation can be explained with given input values -> 0.061223 = 2*(sin(0.286))^2/(1.6+1).

FAQ

What is Non-Dimensional Pressure for High Mach Number?

Non-Dimensional Pressure for High Mach Number is a dimensionless quantity used in aerodynamics to characterize the pressure distribution on a body moving at high speeds, typically at Mach numbers greater than 0.3. It is defined as the ratio of the actual pressure to the dynamic pressure, and it helps in analyzing compressible flow phenomena and is represented as p_mech = 2*(sin(β))^2/(γ+1) or Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1). Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle & 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 Non-Dimensional Pressure for High Mach Number?

Non-Dimensional Pressure for High Mach Number is a dimensionless quantity used in aerodynamics to characterize the pressure distribution on a body moving at high speeds, typically at Mach numbers greater than 0.3. It is defined as the ratio of the actual pressure to the dynamic pressure, and it helps in analyzing compressible flow phenomena is calculated using Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1). To calculate Non-Dimensional Pressure for High Mach Number, you need Wave Angle (β) & Specific Heat Ratio (γ). With our tool, you need to enter the respective value for Wave Angle & Specific Heat Ratio 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