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Supersonic Flying Qualities Experience Using the SR-71Approximately 25 years ago NASA Dryden Flight Research Center, Edwards, California, initiated the evaluation of supersonic handling qualities issues using the XB-70 and the YF-12. Comparison of pilot comments and ratings with some of the classical handling qualities criteria for transport aircraft provided information on the usefulness of these criteria and insight into supersonic flying qualities issues. A second research study has recently been completed which again addressed supersonic flying qualities issues through evaluations of the SR-71 in flight at Mach 3. Additional insight into supersonic flying qualities issues was obtained through pilot ratings and comments. These ratings were compared with existing military specifications and proposed criteria for the High Speed Civil Transport. This paper investigates the disparity between pilot comments and the Neal/Smith criteria through a modification of the technique using vertical speed at the pilot station. The paper specifically addresses the pilot ability to control flightpath and pitch attitude in supersonic flight and pilot displays typical of supersonic maneuvering.
Document ID
19970026105
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Cox, Timothy H.
(NASA Dryden Flight Research Center Edwards, CA United States)
Jackson, Dante
(Analytical Services and Materials, Inc. Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
H-2178
AIAA Paper 97-3654
NAS 1.15:4800
NASA-TM-4800
Meeting Information
Meeting: Atmospheric Flight Mechanics
Location: New Orleans, LA
Country: United States
Start Date: August 11, 1997
End Date: August 13, 1997
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
97N25454
Funding Number(s)
PROJECT: RTOP 529-50-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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