Reduced uncertainties in the flutter analysis of the aerostructures test wing

Reduced uncertainties in the flutter analysis of the aerostructures test wing [electronic resource] / Chan-gi Pak and Shun-fat Lung.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Pak, Chan-gi, 1956-
Corporate Author:	Hugh L. Dryden Flight Research Center
Other Authors:	Lung, Shun-fat
Format:	Government Document Electronic eBook
Language:	English
Published:	Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
Series:	NASA technical memorandum ; 2011-216421.
Subjects:	Flutter analysis. Dynamic structural analysis. Design analysis. Wings. Finite element method. Multidisciplinary design optimization. Flight tests. Dynamic models. Tuning.

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Call Number:	NAS 1.15:2011-216421
NAS 1.15:2011-216421	Available