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

Bibliographic Details

Main Author:	Pak, Chan-gi
Corporate Author:	Hugh L. Dryden Flight Research Center
Other Authors:	Lung, Shun-fat
Format:	Government Document 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.
Online Access:	https://purl.fdlp.gov/GPO/gpo13290