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Finite element analysis and test results comparison for the hybrid wing body center section test article /

Bibliographic Details
Main Author: Przekop, Adam (Author)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2016.
Series:NASA technical memorandum ; 2016-218973.
Subjects:
Critical loading.
Finite element method.
Strain measurement.
Structural stability.
Wings.
Online Access:https://purl.fdlp.gov/GPO/gpo85619
Description
Item Description:"April 2016."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (viii, 106 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 104-105).