METHOD FOR ANALYZING LOAD OF OUTER INSTALLATION OF AIRCRAFT

摘要

PURPOSE: A method for analyzing load of outer installation of aircraft is provided to automatically analyze load of the outer installation of the aircraft. CONSTITUTION: A method comprises the steps of: a step multiplying load factor by load of an installation on the same point to get inertia force; a step multiplying aerodynamic coefficient according to wind tunnel test data by dynamic pressure and area to get aerodynamic force; and multiplying the inertia force by the aerodynamic force after getting the inertia force and the aerodynamic force to calculate load of the installation of the aircraft on the same point.