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analysis and multipoint design of the tca conceptThe goal in this effort is to analyze the baseline TCA concept at transonic and supersonic cruise, then apply the natural flow wing design concept to obtain multipoint performance improvements. Analyses are conducted with OVERFLOW, a Navier-Stokes code for overset grids, using PEGSUS to compute the interpolations between the overset grids.
Document ID
20000058103
Document Type
Conference Paper
Authors
Krist, Steven E.
(NASA Langley Research Center Hampton, VA United States)
Bauer, Steven X. S.
(NASA Langley Research Center Hampton, VA United States)
Buning, Pieter G.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Publication Information
Publication: 1997 NASA High-Speed Research Program Aerodynamic Performance Workshop
Volume: 1
Issue: Part 1
Subject Category
Aircraft Design, Testing and Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20000058091Analytic Primary1997 NASA High-Speed Research Program Aerodynamic Performance Workshop
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