Consider an aircraft flying with a velocity of 450 ft/s at altitude where all the conditions are at standard sea level. At a point on the wing, the velocity is 550 ft/s. Calculate the temperature at this point. Assume Cp is 6006 ft lb/slug R.
Consider an aircraft flying with a velocity of 450 ft/s at altitude where all the conditions are at standard sea level. At a point on the wing, the velocity is 550 ft/s. Calculate the temperature at this point. Assume Cp is 6006 ft lb/slug R.