Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2

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David J. Wing
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Last edited by WorkBot
December 15, 2009 | History

Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2

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Cover of: Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2
Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2
1995, National Aeronautics and Space Administration, Langley Research Center, Available from the National Technical Information Service
in English

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Book Details


Edition Notes

"May 1995."

"Performing organization report number L-17438"--Report documentation page.

Includes bibliographical references (p. 10).

Available electronically at the following URL address: http://techreports.larc.nasa.gov/ltrs/ltrs.html.

WU 505-59-30-04.

Published in
Hampton, Va, Springfield, VA
Series
NASA technical paper -- 3509.
Other Titles
Afterbody nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2.

The Physical Object

Pagination
209 p. :
Number of pages
209

ID Numbers

Open Library
OL17113314M
OCLC/WorldCat
32881803

Source records

Oregon Libraries MARC record

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History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
December 15, 2009 Edited by WorkBot link works
April 22, 2009 Edited by ImportBot add OCLC number
September 27, 2008 Created by ImportBot Imported from Oregon Libraries MARC record