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THE EFFECTS OF SUPERSONIC TRANSPORT FLIGHT CHARACTERISTICS ON PERFORMANCE REQUIREMENTS
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Abstract
This paper discusses possible novel flight characteristics of the supersonic transport, the interrelation of flight characteristics and performance requirements, methods for evaluating the effects of flight characteristics, and examples of how these methods are being used; in SST studies. It also reviews previous flight test experience which may be applicable to the SST, and points out the needs for further research, improved handling qualities, cockpit design, and instrumentation.
Citation
Tymczyszyn, J. and Spiess, P., "THE EFFECTS OF SUPERSONIC TRANSPORT FLIGHT CHARACTERISTICS ON PERFORMANCE REQUIREMENTS," SAE Technical Paper 630243, 1963, https://doi.org/10.4271/630243.Data Sets - Support Documents
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References
- Cooper, George E. Chief Aeronautical Research Pilot - Ames Research Center, NASA, Understanding and Interpreting Pilot Opinion, 25th Annual Meeting, IAS New York January 28 1957
- Geoffrion, D. R. Kibardin, V. M.
- Cheney, Harold K. Engineering Staff Specialist - Flight Test General Dynamics/Convair, A Study of Flight Test Requirements for Takeoff and Landing Certification of the Supersonic Transport A Paper Presented at the 1961 Society of Experimental Test Pilots Symposium
- Shields, E. R. Phelan, D. J. October 1 1953
- White, Maurice D. Schlaff, Bernard M. Drinkwater Fred J. III,
- White, Maurice D. Innis, Robert C.
- Moss, W. W. Gannett, James R. Patten, Paul H. The Supersonic Transport: Pilot Views in Operational Goals, Handling Characteristics and Related Subjects A Paper Presented at the 1961 SAE National Aeronautics Meeting in New York
- Cooper, George E. Chief Research Pilot, NASA Ames Research Center, Moffett Field, California, The Use of Piloted Flight Simulators in Takeoff and Landing Research A Paper Presented to AGARD in Paris January 14–18 1963