Reduced uncertainties in the flutter analysis of the aerostructures test wing /

Reduced uncertainties in the flutter analysis of the aerostructures test wing /

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Bibliographic Details
Author / Creator:Pak, Chʻan-gi.
Imprint:Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
Description:1 online resource (25 p.) : ill., (some col.).
Language:English
Series:NASA/TM ; 2011-216421
NASA technical memorandum ; 2011-216421.
Subject:
Finite element method.
Multidisciplinary design optimization.
Tuning.
Wings (Anatomy)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8535222
Hidden Bibliographic Details
Other authors / contributors:Lung, Shun-fat.
Hugh L. Dryden Flight Research Center
Notes:Title from title screen (viewed on Sept. 27, 2011).
"January 2011."
Includes bibliographical references (p. 13-14).
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2011-216421

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