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Aerodynamics Practice Test: Normal Shock Waves
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Normal Shock Waves topics include: Normal shock equations, flow compressible and its velocity measurement. A normal shock wave is a one-dimensional flow configuration that can be used to study flow behavior and transport processes.  A normal shock wave is a shock with a wave front that is perpendicular to the freestream flow. They occur in supersonic internal and jet flows.  A normal shock wave is the most fundamental type of shock. It is a traveling wave that moves relative to the fluid faster than the local speed of sound.  Here are some characteristics of normal shock waves: Shock... Show more
Aerodynamics Practice Test: Normal Shock Waves
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1 Questions

1. For a non-perfect gas, if we double the pressure while keeping the temperature same, the speed of sound remains the same.