Critical Speed of Sound from Prandtl Relation Solution

STEP 0: Pre-Calculation Summary
Formula Used
Critical Speed of Sound = sqrt(Velocity Downstream of Shock*Velocity Upstream of Shock)
acr = sqrt(V2*V1)
This formula uses 1 Functions, 3 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
Critical Speed of Sound - (Measured in Meter per Second) - The Critical Speed of Sound is defined as the speed of sound at critical conditions in fluid flow.
Velocity Downstream of Shock - (Measured in Meter per Second) - Velocity Downstream of Shock is the velocity of flow behind the shock wave.
Velocity Upstream of Shock - (Measured in Meter per Second) - Velocity Upstream of Shock is the velocity of flow ahead of the shock wave.
STEP 1: Convert Input(s) to Base Unit
Velocity Downstream of Shock: 79.351 Meter per Second --> 79.351 Meter per Second No Conversion Required
Velocity Upstream of Shock: 80.134 Meter per Second --> 80.134 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
acr = sqrt(V2*V1) --> sqrt(79.351*80.134)
Evaluating ... ...
acr = 79.7415389492829
STEP 3: Convert Result to Output's Unit
79.7415389492829 Meter per Second --> No Conversion Required
FINAL ANSWER
79.7415389492829 79.74154 Meter per Second <-- Critical Speed of Sound
(Calculation completed in 00.004 seconds)

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Created by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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Amrita School of Engineering (ASE), Vallikavu
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Normal Shock Relations Calculators

Relation between Mach Number and Characteristic Mach Number
​ LaTeX ​ Go Characteristic Mach Number = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1+2/(Mach Number^2)))^0.5
Downstream Velocity using Prandtl Relation
​ LaTeX ​ Go Velocity Downstream of Shock = (Critical Speed of Sound^2)/Velocity Upstream of Shock
Upstream Velocity using Prandtl Relation
​ LaTeX ​ Go Velocity Upstream of Shock = (Critical Speed of Sound^2)/Velocity Downstream of Shock
Characteristic Mach Number
​ LaTeX ​ Go Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound

Critical Speed of Sound from Prandtl Relation Formula

​LaTeX ​Go
Critical Speed of Sound = sqrt(Velocity Downstream of Shock*Velocity Upstream of Shock)
acr = sqrt(V2*V1)

What is Prandtl relation?

Prandtl relation is an intermediate relation for normal shocks. It relates the velocity ahead of a shock to the downstream velocity after the shock, which in turn help to obtain downstream Mach number of the flow.

How to Calculate Critical Speed of Sound from Prandtl Relation?

Critical Speed of Sound from Prandtl Relation calculator uses Critical Speed of Sound = sqrt(Velocity Downstream of Shock*Velocity Upstream of Shock) to calculate the Critical Speed of Sound, Critical Speed of Sound from Prandtl Relation formula is defined as a relationship that describes the speed at which sound waves propagate through a compressible fluid, particularly in the context of aerodynamics and normal shock waves. Critical Speed of Sound is denoted by acr symbol.

How to calculate Critical Speed of Sound from Prandtl Relation using this online calculator? To use this online calculator for Critical Speed of Sound from Prandtl Relation, enter Velocity Downstream of Shock (V2) & Velocity Upstream of Shock (V1) and hit the calculate button. Here is how the Critical Speed of Sound from Prandtl Relation calculation can be explained with given input values -> 107.2655 = sqrt(79.351*80.134).

FAQ

What is Critical Speed of Sound from Prandtl Relation?
Critical Speed of Sound from Prandtl Relation formula is defined as a relationship that describes the speed at which sound waves propagate through a compressible fluid, particularly in the context of aerodynamics and normal shock waves and is represented as acr = sqrt(V2*V1) or Critical Speed of Sound = sqrt(Velocity Downstream of Shock*Velocity Upstream of Shock). Velocity Downstream of Shock is the velocity of flow behind the shock wave & Velocity Upstream of Shock is the velocity of flow ahead of the shock wave.
How to calculate Critical Speed of Sound from Prandtl Relation?
Critical Speed of Sound from Prandtl Relation formula is defined as a relationship that describes the speed at which sound waves propagate through a compressible fluid, particularly in the context of aerodynamics and normal shock waves is calculated using Critical Speed of Sound = sqrt(Velocity Downstream of Shock*Velocity Upstream of Shock). To calculate Critical Speed of Sound from Prandtl Relation, you need Velocity Downstream of Shock (V2) & Velocity Upstream of Shock (V1). With our tool, you need to enter the respective value for Velocity Downstream of Shock & Velocity Upstream of Shock 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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