How to Calculate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack?
Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack calculator uses Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2 to calculate the Pressure Coefficient, Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack formula is defined as a dimensionless quantity that characterizes the pressure distribution around a shuttle during ascent or re-entry into the Earth's atmosphere, influenced by the angle of attack and blast wave effects. Pressure Coefficient is denoted by Cp symbol.
How to calculate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack using this online calculator? To use this online calculator for Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack, enter Distance from X-Axis (y), Length of Shuttle (l) & Angle of Attack (α) and hit the calculate button. Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack calculation can be explained with given input values -> 0.075147 = 0.0137/(2.2/0.5)+2*(sin(0.190939020168144))^2.