Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers.

摘要

Analytical approaches are considered which might be used to improve and extend current aerodynamic analysis to include the compressibility effects up to and including critical mach numbers. The Rayleigh-Janzen solution is considered for both small disturbance and exact potential flows. A simple numerical method is presented and compared with both experimental results and the results of other analytical methods for potential flow. (Author)