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Unstructured Navier-Stokes Analysis of Full TCA ConfigurationThis paper presents an Unstructured Navier-Stokes Analysis of Full TCA (Technology Concept Airplane) Configuration. The topics include: 1) Motivation; 2) Milestone and approach; 3) Overview of the unstructured-grid system; 4) Results on full TCA W/B/N/D/E configuration; 5) Concluding remarks; and 6) Future directions.
Document ID
20000031541
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Frink, Neal T. (NASA Langley Research Center Hampton, VA United States)
Pirzadeh, Shahyar Z. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Publication Information
Publication: 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop
Volume: 1
Issue: Part 1
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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