Constant G used for Finding Location of Perturbed Shock Calculator

✖Perturbed Shock Location Constant at Normal Force to the perturbed shock, used to find the constant g.ⓘ Perturbed Shock Location Constant at Normal Force [gn]			+10% -10%
✖Perturbed Shock Location Constant at Drag Force to the perturbed shock, used to find the constant g.ⓘ Perturbed Shock Location Constant at Drag Force [gd]			+10% -10%

✖Perturbed Shock Location Constant is a constant that must be determined in order to locate the perturbed shock.ⓘ Constant G used for Finding Location of Perturbed Shock [g]

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Formula

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Constant G used for Finding Location of Perturbed Shock

Formula

`"g" = "gn"/"gd"`

Example

`"6.5"="13"/"2"`

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Constant G used for Finding Location of Perturbed Shock Solution

STEP 0: Pre-Calculation Summary

Formula Used

Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force
g = gn/gd
This formula uses 3 Variables

Variables Used

Perturbed Shock Location Constant - Perturbed Shock Location Constant is a constant that must be determined in order to locate the perturbed shock.
Perturbed Shock Location Constant at Normal Force - Perturbed Shock Location Constant at Normal Force to the perturbed shock, used to find the constant g.
Perturbed Shock Location Constant at Drag Force - Perturbed Shock Location Constant at Drag Force to the perturbed shock, used to find the constant g.

STEP 1: Convert Input(s) to Base Unit

Perturbed Shock Location Constant at Normal Force: 13 --> No Conversion Required
Perturbed Shock Location Constant at Drag Force: 2 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

g = gn/gd --> 13/2

Evaluating ... ...

g = 6.5

STEP 3: Convert Result to Output's Unit

6.5 --> No Conversion Required

FINAL ANSWER

6.5 <-- Perturbed Shock Location Constant

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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< 17 Hypersonic Flow and Disturbances Calculators

Inverse of Density for Hypersonic Flow using Mach Number

Go Inverse of Density = (2+(Specific Heat Ratio-1)*Mach Number^2*sin(Deflection Angle)^2)/(2+(Specific Heat Ratio+1)*Mach Number^2*sin(Deflection Angle)^2)

Coefficient of Pressure with Slenderness Ratio and Similarity Constant

Go Pressure Coefficient = (2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1)

Coefficient of Pressure with Slenderness Ratio

Go Pressure Coefficient = 2/Specific Heat Ratio*Mach Number^2*(Non Dimensionalized Pressure*Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2-1)

Non Dimensional Pressure Equation with Slenderness Ratio

Go Non Dimensionalized Pressure = Pressure/(Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2*Free Stream Pressure)

Density Ratio with Similarity Constant having Slenderness Ratio

Go Density Ratio = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1))*(1/(1+2/((Specific Heat Ratio-1)*Hypersonic Similarity Parameter^2)))

Rasmussen Closed Form Expression for Shock Wave Angle

Go Wave Angle Similarity Parameter = Hypersonic Similarity Parameter*sqrt((Specific Heat Ratio+1)/2+1/Hypersonic Similarity Parameter^2)

Non Dimensional Change in Hypersonic Disturbance Velocity in y Direction

Go Non Dimensional Disturbance Y Velocity = Change in Velocity for Hypersonic Flow y direction/(Freestream Velocity Normal*Slenderness Ratio)

Non Dimensional Change in Hypersonic Disturbance Velocity in x Direction

Go Non Dimensional Disturbance X Velocity = Change in Velocity for Hypersonic Flow/(Freestream Velocity for Blast Wave*Slenderness Ratio^2)

Doty and Rasmussen- Normal Force Coefficient

Go Coefficient of Force = 2*Normal Force/(Density of Fluid*Freestream Velocity Normal^2*Area)

Constant G used for Finding Location of Perturbed Shock

Go Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force

Non Dimensional Velocity Disturbance in y Direction in Hypersonic Flow

Go Non Dimensional Disturbance Y Velocity = (2/(Specific Heat Ratio+1))*(1-1/Hypersonic Similarity Parameter^2)

Non Dimensionalised Time

Go Non Dimensionalized Time = Time/(Length/Freestream Velocity Normal)

Similarity Constant Equation using Wave Angle

Go Wave Angle Similarity Parameter = Mach Number*Wave Angle*180/pi

Change in Velocity for Hypersonic Flow in X Direction

Go Change in Velocity for Hypersonic Flow = Fluid Velocity-Freestream Velocity Normal

Distance from Tip of Leading Edge to Base

Go Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken

Similarity Constant Equation with Slenderness Ratio

Go Hypersonic Similarity Parameter = Mach Number*Slenderness Ratio

Inverse of Density for Hypersonic Flow

Go Inverse of Density = 1/(Density*Wave Angle)

Constant G used for Finding Location of Perturbed Shock Formula

Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force
g = gn/gd

What is shock wave?

Shock wave, strong pressure wave in any elastic medium such as air, water, or a solid substance, produced by supersonic aircraft, explosions, lightning, or other phenomena that create violent changes in pressure.

How to Calculate Constant G used for Finding Location of Perturbed Shock?

Constant G used for Finding Location of Perturbed Shock calculator uses Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force to calculate the Perturbed Shock Location Constant, The Constant g used for finding location of perturbed shock formula is defined as ratio of constant at normal perturbed shock location to constant at perturbed shock location at drag. Perturbed Shock Location Constant is denoted by g symbol.

How to calculate Constant G used for Finding Location of Perturbed Shock using this online calculator? To use this online calculator for Constant G used for Finding Location of Perturbed Shock, enter Perturbed Shock Location Constant at Normal Force (gn) & Perturbed Shock Location Constant at Drag Force (gd) and hit the calculate button. Here is how the Constant G used for Finding Location of Perturbed Shock calculation can be explained with given input values -> 1.5 = 13/2.

FAQ

What is Constant G used for Finding Location of Perturbed Shock?

The Constant g used for finding location of perturbed shock formula is defined as ratio of constant at normal perturbed shock location to constant at perturbed shock location at drag and is represented as g = gn/gd or Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force. Perturbed Shock Location Constant at Normal Force to the perturbed shock, used to find the constant g & Perturbed Shock Location Constant at Drag Force to the perturbed shock, used to find the constant g.

How to calculate Constant G used for Finding Location of Perturbed Shock?

The Constant g used for finding location of perturbed shock formula is defined as ratio of constant at normal perturbed shock location to constant at perturbed shock location at drag is calculated using Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force. To calculate Constant G used for Finding Location of Perturbed Shock, you need Perturbed Shock Location Constant at Normal Force (gn) & Perturbed Shock Location Constant at Drag Force (gd). With our tool, you need to enter the respective value for Perturbed Shock Location Constant at Normal Force & Perturbed Shock Location Constant at Drag Force and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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