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An Experimental Database for Conventional and Alternate Control Concepts on the HSR 1.675% Reference H ModelThe objective was to experimentally evaluate the longitudinal and lateral-directional stability and control characteristics of the Reference H configuration at supersonic and transonic speeds. A series of conventional and alternate control devices were also evaluated at supersonic and transonic speeds. A database on the conventional and alternate control devices was to be created for use in the HSR program.
Document ID
20000044875
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
McMillin, Naomi
(NASA Langley Research Center Hampton, VA United States)
Allen, Jerry
(NASA Langley Research Center Hampton, VA United States)
Erickson, Gary
(NASA Langley Research Center Hampton, VA United States)
Campbell, Jim
(NASA Langley Research Center Hampton, VA United States)
Mann, Mike
(NASA Langley Research Center Hampton, VA United States)
Kubiatko, Paul
(McDonnell-Douglas Aerospace United States)
Yingling, David
(McDonnell-Douglas Aerospace United States)
Mason, Charlie
(Lockheed Martin Aerospace United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Publication Information
Publication: First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop
Issue: Part 3
Subject Category
Aircraft Stability And Control
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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