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TLNS3D/CDISC Multipoint Design of the TCA ConceptThis paper presents the work done to date by the authors on developing an efficient approach to multipoint design and applying it to the design of the HSR TCA configuration. While the title indicates that this exploratory study has been performed using the TLNS3DMB flow solver and the CDISC design method, the CDISC method could have been used with any flow solver, and the multipoint design approach does not require the use of CDISC. The goal of the study was to develop a multipoint design method that could achieve a design in about the same time as 10 analysis runs.
Document ID
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Campbell, Richard L.
(NASA Langley Research Center Hampton, VA United States)
Mann, Michael J.
(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
Work of the US Gov. Public Use Permitted.
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