The mixed elliptic-hyperbolic relaxation method for obtaining steady-state solutions to two-dimensional transonic potential equations is extended to the transonic small disturbance equation in three dimensions. In particular, transonic flow is considered both about nonlifting wing-cylinder combinations and over thin lifting wings with sweep and taper. The treatment is restricted to freestream Mach numbers less than one and to wings with subsonic trailing edges.
Relaxation methods for transonic flow about wing-cylinder combinations and lifting swept wings
International Conference on Numerical Methods in Fluid Mechanics ; 1972 ; Paris, France
1973-01-01
Miscellaneous
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English
Transonic flow about lifting wing-body combinations
AIAA | 1974
|Transonic flow about lifting wing-body combinations
NTRS | 1974
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