Critical pressure coefficient with respect to critical Mach number Calculator

The critical pressure coefficient with respect to the critical Mach number () is a parameter used in aerodynamics to describe the pressure coefficient () at which the flow over an airfoil or aerodynamic surface reaches a critical condition associated with the critical Mach number (). It provides insights into the behavior of the flow as it approaches and passes the critical Mach number. 

  • Specific heat ratio (γ)
  • Critical Mach number (Mcr)
  • Critical pressure coefficient (Cp,cr)

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