Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

Computational test cases for a clipped delta ...
Robert M. Bennett
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Last edited by VacuumBot
August 13, 2012 | History

Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

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Cover of: Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
1999, National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor
Microform in English

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Book Details


Edition Notes

Shipping list no.: 99-0729-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.

Published in
Hampton, Va, Springfield, VA
Series
[NASA technical memorandum] -- NASA/TM-1999-209104, NASA technical memorandum -- 209104..

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL17133246M

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Download catalog record: RDF / JSON / OPDS | Wikipedia citation
August 13, 2012 Edited by VacuumBot Updated format '[microform] /' to 'Microform'; Removed author from Edition (author found in Work)
December 15, 2009 Edited by WorkBot link works
September 27, 2008 Created by ImportBot Imported from bcl_marc record