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 method 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
1987-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 1993
|Transonic Propulsion Aerodynamics Research at NASA Langley Research Center
SAE Technical Papers | 1992
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