Shock Strength Formula

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Shock Strength is mathematically the difference in pressure across a normal shockwave to the pressure ahead of a shockwave. Check FAQs
Δpstr=(2γ1+γ)(M12-1)
Δpstr - Shock Strength?γ - Specific Heat Ratio?M1 - Mach Number Ahead of Normal Shock?

Shock Strength Example

With values
With units
Only example

Here is how the Shock Strength equation looks like with Values.

Here is how the Shock Strength equation looks like with Units.

Here is how the Shock Strength equation looks like.

1.4235Edit=(21.4Edit1+1.4Edit)(1.49Edit2-1)
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Shock Strength Solution

Follow our step by step solution on how to calculate Shock Strength?

FIRST Step Consider the formula
Δpstr=(2γ1+γ)(M12-1)
Next Step Substitute values of Variables
Δpstr=(21.41+1.4)(1.492-1)
Next Step Prepare to Evaluate
Δpstr=(21.41+1.4)(1.492-1)
Next Step Evaluate
Δpstr=1.42345
LAST Step Rounding Answer
Δpstr=1.4235

Shock Strength Formula Elements

Variables
Shock Strength
Shock Strength is mathematically the difference in pressure across a normal shockwave to the pressure ahead of a shockwave.
Symbol: Δpstr
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Specific Heat Ratio
The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume.
Symbol: γ
Measurement: NAUnit: Unitless
Note: Value should be between 1 to 2.
Mach Number Ahead of Normal Shock
Mach Number Ahead of Normal Shock represents the velocity of a fluid or airflow relative to the speed of sound before encountering a normal shock wave.
Symbol: M1
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.

Other formulas in Property Change Across Shock Waves category

​Go Entropy Change across Normal Shock
ΔS=Rln(p01p02)
​Go Density Ratio across Normal Shock
ρr=(γ+1)M122+(γ-1)M12
​Go Pressure Ratio across Normal Shock
Pr=1+2γγ+1(M12-1)
​Go Temperature Ratio across Normal Shock
Tr=1+(2γγ+1)(M12-1)(γ+1)M122+((γ-1)M12)

How to Evaluate Shock Strength?

Shock Strength evaluator uses Shock Strength = ((2*Specific Heat Ratio)/(1+Specific Heat Ratio))*(Mach Number Ahead of Normal Shock^2-1) to evaluate the Shock Strength, The Shock Strength calculates the strength of a normal shock wave in a fluid flow. This formula incorporates the ratio of specific heats for the fluid and the Mach number ahead of the shock to determine the shock strength. It provides insight into the intensity of the shock wave, aiding in the analysis of compressible flow behavior and its impact on fluid dynamics. Shock Strength is denoted by Δpstr symbol.

How to evaluate Shock Strength using this online evaluator? To use this online evaluator for Shock Strength, enter Specific Heat Ratio (γ) & Mach Number Ahead of Normal Shock (M1) and hit the calculate button.

FAQs on Shock Strength

What is the formula to find Shock Strength?
The formula of Shock Strength is expressed as Shock Strength = ((2*Specific Heat Ratio)/(1+Specific Heat Ratio))*(Mach Number Ahead of Normal Shock^2-1). Here is an example- 1.42345 = ((2*1.4)/(1+1.4))*(1.49^2-1).
How to calculate Shock Strength?
With Specific Heat Ratio (γ) & Mach Number Ahead of Normal Shock (M1) we can find Shock Strength using the formula - Shock Strength = ((2*Specific Heat Ratio)/(1+Specific Heat Ratio))*(Mach Number Ahead of Normal Shock^2-1).
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