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.
Calculation of Unsteady Subsonic and Supersonic Flow about Oscillating Wings and Bodies by New Panel Methods
1989
25 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Panel method(Fluid dynamics) , Wings , Subsonic flow , Supersonic flow , Aerodynamic loads , Oscillations , Aerodynamic configurations , Unsteady flow , Damping , External stores , Fighter aircraft , Aircraft design , Computational fluid dynamics , Mathematical models , Wing body configurations , Foreign technology
Oscillating wings in compressible subsonic flow
TIBKAT | 1957
|Oscillating wings in compressible subsonic flow
SLUB | 1957
|