Compute for the Mach number of an aircraft flying with a velocity of 150 m/s with all the aerodynamic quantities are at sea level condition. Assume the value of the specific gas constant and specific heat ratio is 287.08 J/Kg K and 1.39.
Compute for the Mach number of an aircraft flying with a velocity of 150 m/s with all the aerodynamic quantities are at sea level condition. Assume the value of the specific gas constant and specific heat ratio is 287.08 J/Kg K and 1.39.