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Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary designProgress in the development of computational methods for steady and unsteady aerodynamics has perennially paced advancements in aeroelastic analysis and design capabilities. Since these capabilities are of growing importance in the analysis and design of high-performance aircraft, considerable effort has been directed toward the development of appropriate aerodynamic methodology. The contributions to those efforts from the integral-equations research program at the NASA Langley Research Center is reviewed. Specifically, the current scope, progress, and plans for research and development for inviscid and viscous flows are discussed, and example applications are shown in order to highlight the generality, versatility, and attractive features of this methodology.
Document ID
Document Type
Conference Paper
Yates, E. Carson, Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1990
Subject Category
Report/Patent Number
NAS 1.15:102677
Meeting Information
Japan/USA Boundary Elements Symposium(Palo Alto, CA)
Funding Number(s)
PROJECT: RTOP 505-63-01
Distribution Limits
Work of the US Gov. Public Use Permitted.

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