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Supersonic Flying Qualities Experience Using the SR-71

Cox, Timothy H. and Jackson, Dante (1997) Supersonic Flying Qualities Experience Using the SR-71. Technical Report NASA TM-4800, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

Approximately 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.

EPrint Type:NASA Technical Memorandum
Keywords:Bandwidth criteria, Flightpath bandwidth, Flying qualities, High Speed Civil Transport, Neal/Smith criteria, SR-71 aircraft, Supersonic flying qualities
Subjects:Aircraft/Project: SR-71 Blackbird
(01 - 09) Aeronautics: (08) Aircraft Stability And Control
ID Code:125
Deposited On:07 June 2004
Additional Information:16 pages. Presented at the AIAA Atmospheric Flight Mechanics Conference New Orleans, Louisiana, August 11–13, 1997, AIAA 97-3654
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Last Modified: September 14, 2004
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