An aircraft is flying with a velocity of 90 m/s. Compute for the mach number if the pressure and density is at standard sea level condition. Assume R is at standard condition. K is 1.4.
An aircraft is flying with a velocity of 90 m/s. Compute for the mach number if the pressure and density is at standard sea level condition. Assume R is at standard condition. K is 1.4.