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, The Pressure coefficient combined with blast wave for shuttle at angle of attack formula is defined as the inverse of ratio of the distance from the tip of shuttle to the length of the shuttle plus double the square of angle of attack. 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.