1. The problem statement, all variables and given/known data A Pitot is used to measure the air speed of a light aircraft. The pressure difference recorded by the tube in flight was 3300 N/m^2. The local air pressure was 950 kN/m^2 and the temperature was 7 Degrees (280K). Calculate the local air density and the speed of the aircraft. 2. Relevant equations Not sure if relevent but aattempted to use this formula: p+1/2pV^2+pgh= constant 3. The attempt at a solution Attempting as of right now any help appreciated.