L = mg sec p = 36 200 / cos(_30o ) = 44 1 LO The reference lift is the weight so AL = 44 100 _ 38 200 = 5 900 1b. The pitching moment is zero, else there would be a pitching acceleration and non-steady flight. The dynamic pressure is calculated to be q = 175 .51b/ ft2. S = 542 .5 ft2 so A CL = 0.062 and Co =0. In the given equations &=0, AM =0, but q =0. We get q from the kinematic equations, e.g. equation 4.5 with the right symbols. q = sin ocos ey + cos 60 = sin ou