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Model 2b Test ResultsThis activity is part of the Wind Tunnel Database and Wind Tunnel Data Corrections Programs. The main purpose of this test was to evaluate the aerodynamic performance of the TCA Baseline configuration around the supersonic cruise point.
Document ID
20000038431
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Goodsell, Aga M. (NASA Ames Research Center Moffett Field, CA 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 2
Subject Category
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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