The object of the work was to investigate the feasibility of using polynomial approximation techniques for the digital solution of air data formulae. Least square methods were used to obtain polynomial approximations to the air data formulae for height, Mach number, indicated airspeed and true ...
Question: Explain how limit load factors change with changes in aircraft weight. Support your answer with formula work and/or calculation example. Load Factor: It is defined as the ratio of the maximum load sustain by an aircraft to t...