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V/STOL status from the engine technology viewpointDirections for designs and powerplant configurations for V/STOL aircraft are explored. The Harrier is the only V/STOL aircraft in service, having performed for over 12 yr. Rolls-Royce has studied engines with powered lift separation from forward propulsion, and engines with composite lift/propulsion modes, resulting in concentration on vectored thrust using rotating or deflected nozzles. The necessity for higher combat performance creates a need for higher specific thrust for supersonic flight (Mach 2), which is achievable with plenum chamber burning. The core flows are exhausted through separate nozzle systems for independent control. Intake in a V/STOL follows a short path and results in nonuniform flow, and testing is described to account for the effects of nonuniform static pressures and temperatures.
Document ID
19820033378
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lewis, G. M.
Lewis, W. J.
(Rolls-Royce, Ltd. Bristol, United Kingdom)
Date Acquired
August 10, 2013
Publication Date
December 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 81-2648
Report Number: AIAA PAPER 81-2648
Meeting Information
Meeting: V/STOL Conference
Location: Palo Alto, CA
Start Date: December 7, 1981
End Date: December 9, 1981
Sponsors: American Institute of Aeronautics and Astronautics and NASA Ames Research Center
Accession Number
82A16913
Distribution Limits
Public
Copyright
Other

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