The supersonic flow over a blunt body is given. Mark the area where the normal shock wave exists.

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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

The supersonic flow over a blunt body is given. Mark the area where the normal shock wave exists.<br /><img src='https://www.fatskills.com/engineering/aerodynamics-questions-answers-basic-normal-shock-equations-q2.png' alt='Find where the normal shock wave of supersonic flow exists in given blunt body' width='406' height='292' class='alignnone size-full wp-image-300998' />