The current scope, recent progress, and plans for research and development of computational methods for unsteady aerodynamics at the NASA Langley Research Center are reviewed. Both integral equations and finite difference methods for inviscid and viscous flows are discussed. Although the great bulk of the effort has focused on finite difference solution of the transonic small perturbation equation, the integral equation program is given primary emphasis here because it is less well known.
Development of computational methods for unsteady aerodynamics at the NASA Langley Research Center
1987-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 1993
|Transonic Propulsion Aerodynamics Research at NASA Langley Research Center
SAE Technical Papers | 1992
|