Determination of Non-Linear Dynamic Aerodynamic Coefficients for Aircraft

摘要

In order to accurately predict the flight dynamics of fighter aircraft, arelatively complete data base for static and dynamic aerodynamics properties for a complete range of flight conditions is required. Since it is impossible to acquire a complete data base for all possible combinations of aircraft attitude and motion parameters, the available data base must be interpolated between test data points for conditions that were not specifically tested. This requires an