This volume presents three computer programs that calculate the generalized aerodynamic forces for the three flight regimes: Subsonic Flight, Transonic Flight, Supersonic Flight and may be used with the Modal Flutter Analysis Program of Vol. III. The subsonic program is based upon Kernel Function formulation. The transonic and supersonic programs are based upon the Mach Box technique. (Author)
Collocation Flutter Analysis Study II (COFA II). Volume II. Unsteady Aerodynamic Generalized Force Programs for Subsonic, Transonic, and Supersonic Flight Regimes
1970
102 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Fluid Mechanics , Aerospace planes , Aerodynamic control surfaces , Flutter , Aerodynamic characteristics , Mathematical models , Vibration , Resonant frequency , Subsonic characteristics , Transonic characteristics , Supersonic characteristics , Aerodynamic loading , Theory , Computer programs , Computer programming , Collocation flutter
Aerodynamic Design of Swept Infinite Wing with Flap for Subsonic and Transonic Flight Regimes
British Library Conference Proceedings | 1996
|Aerodynamic Design of Swept Infinite Wing with Flap for Subsonic and Transonic Flight Regimes
British Library Online Contents | 1996
|