Temperature Ratio for Unsteady Compression Waves Solution

STEP 0: Pre-Calculation Summary
Formula Used
Temperature Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^2
Tratio = (1+((γ-1)/2)*(u'/cspeed))^2
This formula uses 4 Variables
Variables Used
Temperature Ratio - Temperature ratio is the ratio of temperatures at different instances of any process or environment.
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.
Induced Mass Motion - (Measured in Kilogram Square Meter) - Induced Mass Motion, added mass or virtual mass is the inertia added to a system because an accelerating or decelerating body must move some volume of surrounding fluid as it moves through it.
Speed of Sound - (Measured in Meter per Second) - The speed of sound is defined as the dynamic propagation of sound waves.
STEP 1: Convert Input(s) to Base Unit
Specific Heat Ratio: 1.6 --> No Conversion Required
Induced Mass Motion: 8.5 Kilogram Square Meter --> 8.5 Kilogram Square Meter No Conversion Required
Speed of Sound: 343 Meter per Second --> 343 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Tratio = (1+((γ-1)/2)*(u'/cspeed))^2 --> (1+((1.6-1)/2)*(8.5/343))^2
Evaluating ... ...
Tratio = 1.01492407500276
STEP 3: Convert Result to Output's Unit
1.01492407500276 --> No Conversion Required
FINAL ANSWER
1.01492407500276 1.014924 <-- Temperature Ratio
(Calculation completed in 00.020 seconds)

Credits

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Indian Institute of Technology (IIT), Bombay
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Compression Waves Calculators

Density before Shock Formation for Compression 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 for Compression 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))
Temperature Ratio for Unsteady Compression Waves
​ LaTeX ​ Go Temperature Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^2

Temperature Ratio for Unsteady Compression Waves Formula

​LaTeX ​Go
Temperature Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^2
Tratio = (1+((γ-1)/2)*(u'/cspeed))^2

What is an induced mass motion?

In fluid mechanics, added mass or virtual mass is the inertia added to a system because an accelerating or decelerating body must move (or deflect) some volume of surrounding fluid as it moves through it

How to Calculate Temperature Ratio for Unsteady Compression Waves?

Temperature Ratio for Unsteady Compression Waves calculator uses Temperature Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^2 to calculate the Temperature Ratio, Temperature Ratio for Unsteady Compression Waves formula is defined as a dimensionless quantity that characterizes the temperature change across a compression wave in hypersonic inviscid flow, providing a crucial parameter in the analysis of high-speed compressible flows and their applications in aerospace engineering. Temperature Ratio is denoted by Tratio symbol.

How to calculate Temperature Ratio for Unsteady Compression Waves using this online calculator? To use this online calculator for Temperature Ratio for Unsteady Compression Waves, enter Specific Heat Ratio (γ), Induced Mass Motion (u') & Speed of Sound (cspeed) and hit the calculate button. Here is how the Temperature Ratio for Unsteady Compression Waves calculation can be explained with given input values -> 1.014924 = (1+((1.6-1)/2)*(8.5/343))^2.

FAQ

What is Temperature Ratio for Unsteady Compression Waves?
Temperature Ratio for Unsteady Compression Waves formula is defined as a dimensionless quantity that characterizes the temperature change across a compression wave in hypersonic inviscid flow, providing a crucial parameter in the analysis of high-speed compressible flows and their applications in aerospace engineering and is represented as Tratio = (1+((γ-1)/2)*(u'/cspeed))^2 or Temperature Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/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, Induced Mass Motion, added mass or virtual mass is the inertia added to a system because an accelerating or decelerating body must move some volume of surrounding fluid as it moves through it & The speed of sound is defined as the dynamic propagation of sound waves.
How to calculate Temperature Ratio for Unsteady Compression Waves?
Temperature Ratio for Unsteady Compression Waves formula is defined as a dimensionless quantity that characterizes the temperature change across a compression wave in hypersonic inviscid flow, providing a crucial parameter in the analysis of high-speed compressible flows and their applications in aerospace engineering is calculated using Temperature Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^2. To calculate Temperature Ratio for Unsteady Compression Waves, you need Specific Heat Ratio (γ), Induced Mass Motion (u') & Speed of Sound (cspeed). With our tool, you need to enter the respective value for Specific Heat Ratio, Induced Mass Motion & 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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