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Computational Simulations for Stability and Control: BCA State-of-the-ArtThe presentation will show some of our recent work in using the NASA-built Navier-Stokes solvers for various applications including airplane control surface effectiveness study, Reynolds number scaling, and high lift configuration analysis.
Document ID
20040086518
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Yu, N. J. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Kao, T. J. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Bogue, D. R. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Lines, T. R. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2004
Publication Information
Publication: COMSAC: Computational Methods for Stability and Control, Part 2
Subject Category
Computer Programming And Software
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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