Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft by Barbara S. Esker

Cover of: Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft | Barbara S. Esker

Published by NASA, For sale by the National Technical Information Service in [Washington, D.C.], [Springfield, Va .

Written in English

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Subjects:

  • Airplanes -- Ramjet engines -- Nozzles,
  • Short take-off and landing aircraft -- Jet propulsion

Edition Notes

Book details

StatementBarbara S. Esker and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, ASME, SAE, and ASEE, Orlando, Florida, July 16-18, 1990.
SeriesNASA technical memorandum -- 103120.
ContributionsMcArdle, Jack G., United States. National Aeronautics and Space Administration.
The Physical Object
Pagination10 p. :
Number of Pages10
ID Numbers
Open LibraryOL17630526M
OCLC/WorldCa24990569

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Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft by Barbara S.

Esker,NASA, For sale by the National Technical Information Service edition, in Pages: Get this from a library. Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft. [Barbara S Esker; Jack G McArdle; United.

A short take-off and vertical landing aircraft (STOVL aircraft) is a fixed-wing aircraft that is able to take off from a short runway (or take off vertically if it does not have a heavy payload) and land vertically (i.e.

with no runway). The formal NATO definition (since ) is. A Short Take-Off and Vertical Landing aircraft is a fixed-wing aircraft capable of clearing a 15 m (50 ft. Full text of "NASA Technical Reports Server (NTRS) Bibliography of Lewis Research Center technical publications announced in " See other formats.

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