The Linearized Supersonic Pressure Coefficient, often denoted as , is a term used in aerodynamics to describe the pressure distribution around an object moving at supersonic speeds. It provides a measure of how the local pressure at a specific point on the object’s surface deviates from the freestream pressure.
- Pressure coefficient (Cp)
- Angle (θ) in rad
- Freestream Mach number (M∞) in m/s