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Thrust Nozzles for Supersonic Transport Aircraft FREE

[+] Author Affiliations
David Migdal, John J. Horgan

Pratt and Whitney Aircraft, East Hartford, CT

Paper No. 63-AHGT-73, pp. V001T01A022; 11 pages
doi:10.1115/63-AHGT-73
From:
  • ASME 1963 Aviation and Space, Hydraulic, and Gas Turbine Conference and Products Show
  • ASME 1963 Aviation and Space, Hydraulic, and Gas Turbine Conference and Products Show
  • Los Angeles, California, USA, March 3–7, 1963
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7992-4
  • Copyright © 1963 by ASME

abstract

Supersonic transports will require jet-engine thrust nozzles that are highly efficient from take-off to supersonic cruise in order to minimize the direct operating costs. Variable-area ejectors, plug nozzles, and modifications of these basic types have been tested extensively during the past several years. Performance trends for these nozzles are presented with the emphasis on external flow effects. A new ejector which utilizes aerodynamically actuated doors to admit external air into the ejector shroud is discussed.

Copyright © 1963 by ASME
Topics: Thrust , Nozzles , Aircraft
This article is only available in the PDF format.

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