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Propulsion Systems for Supersonic V/STOL Aircraft FREE

[+] Author Affiliations
W. J. Lewis

Rolls-Royce plc, Bristol, England

Paper No. 89-GT-309, pp. V002T02A010; 7 pages
doi:10.1115/89-GT-309
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7914-6
  • Copyright © 1989 by ASME

abstract

A number of different powerplant systems have been and are being considered for supersonic V/STOL aircraft. Some of the main features of these different powerplants are described. As a result of studying the results of operation of successful and unsuccessful V/STOL aircraft in the powered lift condition, a number of real requirements for practical and flexible operation can be identified. These requirements may have a profound impact on the design and configuration of the powered lift powerplant. Some of these are discussed and conclusions reached.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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