Calculation of Unsteady Subsonic and Supersonic Flow about Oscillating Wings and Bodies by New Panel Methods.

摘要

Unsteady aerodynamic loads in the subsonic and supersonic domain have been obtained with two new panel methods for lifting surfaces and for realistic aircraft configurations. A description of the methods is given. Results are presented and comparisons are made with results of existing methods and with experimental data for a fighter-type wing with external stores.