High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

High-Reynolds-number test of a 5-percent-thic ...
Julio Chu
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Last edited by VacuumBot
August 9, 2012 | History

High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

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Cover of: High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
1990, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English
Cover of: High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
1990, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English
Cover of: High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
1990, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English
Cover of: High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
1990, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English

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Book Details


Edition Notes

Distributed to depository libraries in microfiche.

Shipping list no.: 93-1213-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 3 microfiches.

Published in
[Washington, DC], [Springfield, Va
Series
NASA technical memorandum -- 4189.
Other Titles
High Reynolds number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions., High-Reynolds-number test of a five-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wind tunnel distributions.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL18069157M

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Download catalog record: RDF / JSON / OPDS | Wikipedia citation
August 9, 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
October 9, 2008 Created by ImportBot Imported from Oregon Libraries MARC record