Pressure coefficient behind an oblique shock wave in the hypersonic limit Calculator

The pressure coefficient behind an oblique shock wave is a dimensionless quantity that measures the relative change in pressure on the surface of a body due to the oblique shock wave that forms when the body is at an angle to the supersonic or hypersonic flow. 

  • Pressure coefficient (Cp)
  • Specific heat ratio (𝛾)
  • Oblique shock angle (β) in rad

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