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Effects of atmospheric conditions on the operating characteristics of supersonic cruise aircraftSince for maximum range a supersonic transport must cruise near its maximum Mach number, accurate flight control is needed, especially when severe atmospheric transients are encountered. This paper describes atmospheric transients that have been encountered by the XB-70, YF-12, and Concorde aircraft during supersonic flights and the ensuing responses of the aircraft propulsion and flight control systems. It was found that atmospheric conditions affected these supersonic cruise vehicles in much the same way, with minor differences according to the type of propulsion and flight control system. Onboard sensors are sufficiently accurate to provide data on the atmosphere, including turbulence over the route, that are accurate enough for entry in the climatic record and for use as inputs to the control systems. Nominal atmospheric transients can be satisfactorily controlled, but some problems remain for extreme cases.
Document ID
19770028060
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schweikhard, W. G.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Gilyard, G. B.
(NASA Flight Research Center Edwards, Calif., United States)
Talbot, J. E.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Brown, T. W.
(British Aircraft Co. Bristol, United Kingdom)
Date Acquired
August 8, 2013
Publication Date
October 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 76-112
Meeting Information
Meeting: International Astronautical Congress
Location: Anaheim, CA
Start Date: October 10, 1976
End Date: October 16, 1976
Sponsors: International Astronautical Federation
Accession Number
77A10912
Distribution Limits
Public
Copyright
Other

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