Ratio of New and Old Temperature for Expansion Waves Solution

STEP 0: Pre-Calculation Summary
Formula Used
Temperature Ratio across Shock = (1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2)
Tshockratio = (1-((γ-1)/2)*(Vn/cold))^(2)
This formula uses 4 Variables
Variables Used
Temperature Ratio across Shock - Temperature ratio across shock is the ratio of downstream temperature to upstream temperature across the shock wave.
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.
Normal velocity - (Measured in Meter per Second) - Normal velocity is the velocity normal to the shock formation.
Old Speed of Sound - (Measured in Meter per Second) - Old speed of sound is the speed of sound before the shock.
STEP 1: Convert Input(s) to Base Unit
Specific Heat Ratio: 1.6 --> No Conversion Required
Normal velocity: 1000 Meter per Second --> 1000 Meter per Second No Conversion Required
Old Speed of Sound: 342 Meter per Second --> 342 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Tshockratio = (1-((γ-1)/2)*(Vn/cold))^(2) --> (1-((1.6-1)/2)*(1000/342))^(2)
Evaluating ... ...
Tshockratio = 0.0150815635580178
STEP 3: Convert Result to Output's Unit
0.0150815635580178 --> No Conversion Required
FINAL ANSWER
0.0150815635580178 0.015082 <-- Temperature Ratio across Shock
(Calculation completed in 00.004 seconds)

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Expansion Waves Calculators

Density before Shock Formation for Expansion Wave
​ LaTeX ​ Go Density Behind Shock = Stagnation pressure ahead of shock/(1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-Time in Seconds))
New Pressure after Shock Formation, Subtracted to Velocity for Expansion Wave
​ LaTeX ​ Go Pressure = Density Ahead of Shock*(1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-Time in Seconds))
Pressure Ratio for Unsteady Waves with Subtracted Induced Mass Motion for Expansion Waves
​ LaTeX ​ Go Pressure Ratio = (1-((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-1))
Ratio of New and Old Temperature for Expansion Waves
​ LaTeX ​ Go Temperature Ratio across Shock = (1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2)

Ratio of New and Old Temperature for Expansion Waves Formula

​LaTeX ​Go
Temperature Ratio across Shock = (1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2)
Tshockratio = (1-((γ-1)/2)*(Vn/cold))^(2)

What is specific heat ratio?

In thermal physics and thermodynamics, the heat capacity ratio, also known as the adiabatic index, the ratio of specific heats, or Laplace's coefficient, is the ratio of the heat capacity at constant pressure (CP) to heat capacity at constant volume (CV).

How to Calculate Ratio of New and Old Temperature for Expansion Waves?

Ratio of New and Old Temperature for Expansion Waves calculator uses Temperature Ratio across Shock = (1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2) to calculate the Temperature Ratio across Shock, Ratio of New and Old Temperature for Expansion Waves formula is defined as a dimensionless quantity that characterizes the temperature ratio across an expansion wave in hypersonic inviscid flow, providing a crucial parameter in understanding the flow behavior and its effects on the surrounding environment. Temperature Ratio across Shock is denoted by Tshockratio symbol.

How to calculate Ratio of New and Old Temperature for Expansion Waves using this online calculator? To use this online calculator for Ratio of New and Old Temperature for Expansion Waves, enter Specific Heat Ratio (γ), Normal velocity (Vn) & Old Speed of Sound (cold) and hit the calculate button. Here is how the Ratio of New and Old Temperature for Expansion Waves calculation can be explained with given input values -> 0.015082 = (1-((1.6-1)/2)*(1000/342))^(2).

FAQ

What is Ratio of New and Old Temperature for Expansion Waves?
Ratio of New and Old Temperature for Expansion Waves formula is defined as a dimensionless quantity that characterizes the temperature ratio across an expansion wave in hypersonic inviscid flow, providing a crucial parameter in understanding the flow behavior and its effects on the surrounding environment and is represented as Tshockratio = (1-((γ-1)/2)*(Vn/cold))^(2) or Temperature Ratio across Shock = (1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2). 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, Normal velocity is the velocity normal to the shock formation & Old speed of sound is the speed of sound before the shock.
How to calculate Ratio of New and Old Temperature for Expansion Waves?
Ratio of New and Old Temperature for Expansion Waves formula is defined as a dimensionless quantity that characterizes the temperature ratio across an expansion wave in hypersonic inviscid flow, providing a crucial parameter in understanding the flow behavior and its effects on the surrounding environment is calculated using Temperature Ratio across Shock = (1-((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2). To calculate Ratio of New and Old Temperature for Expansion Waves, you need Specific Heat Ratio (γ), Normal velocity (Vn) & Old Speed of Sound (cold). With our tool, you need to enter the respective value for Specific Heat Ratio, Normal velocity & Old Speed of Sound 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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