Neglecting air resistance and the weight of the propellant, determine the work done in propelling a 13-ton satellite to a height of 300miles above Earth and 550miles above earth.
Assume Earth has a radius of 4000miles.
Can someone please show me how to do this?
A body moves through air at a velocity of 200 m/s. The pressure and temperature in
the air upstream of the body are 100 kPa and 30◦ C respectively. Find the pressure
at a point on the body where the velocity of the air relative to the body is zero (1)
accouting for compressibility and (2)...