An indirect method for finding shock-free airfoils and a nearly direct method for finding shock-free airfoils and wing are discussed. While the mathematics of both procedures is emphasized, illustrative practical results are given. (Author)
Shock-Free Configurations in Two- and Three- Dimensional Transonic Flow
1981
22 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Airfoils , Wings , Aerodynamic configurations , Shock waves , Transonic flow , Fluid dynamics , Shape , Mathematical models , Algorithms , Computerized simulation , Applied mathematics , Two dimensional , Three dimensional , Jet aircraft , Turbojet engines , Shock free airfoils
New method for designing shock-free transonic configurations
Tema Archiv | 1979
|Transonic flow about lifting configurations.
NTRS | 1973
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