The pressure coefficient at the location of minimum pressure, denoted as “Cp,A,” is an aerodynamic parameter that describes the pressure distribution on the surface of an object, typically an airfoil or wing, at the specific point where the pressure is at its minimum value.
- Pressure coefficient at minimum pressure (Cp,A)
- Specific heat ratio (γ)
- Freestream Mach number (M∞)
- Mach number at minium pressure (MA)