Overturning moment studies for APT-E (IM-AERO-032)

Wind tunnel tests on a 1/24 scale model APT-E at yaw andles between 40 and 50 degrees and roll angles between 15 and -15 degrees are reported. The aerodynamic coefficients of lift, side force and overturning moment obtained from the tests are given in Table 1 and values of overturning...