Development of computational methods for unsteady aerodynamics at the NASA Langley Research CenterThe 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.
Document ID
19870019086
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yates, E. Carson, Jr. (NASA Langley Research Center Hampton, VA, United States)
Whitlow, Woodrow, Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1987
Publication Information
Publication: AGARD, Future Research on Transonic Unsteady Aerodynamics and Its Aeroelastic Applications