Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /

Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /

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Bibliographic Details
Author / Creator:Erickson, Gary E., author.
Imprint:Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
Description:1 online resource (50 pages) : illustrations.
Language:English
Series:NASA/TM 2013-217977
NASA technical memorandum ; 217977.
Subject:
Mach number.
Reynolds number.
Trailing edge flaps.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/9785828
Hidden Bibliographic Details
Other authors / contributors:United States. National Aeronautics and Space Administration, sponsoring body.
Langley Research Center, issuing body.
Notes:Title from title screen (viewed Oct. 18, 2013).
"April 2013."
Includes bibliographical references (pages 9-10).
L-20228
Sponsored by the National Aeronautics and Space Administration, Washington, DC 122711.03.07.07.16.80
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2013-217977

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