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Plan, formulate, discuss and correlate a NASTRAN finite element vibrations model of the Boeing Model 360 helicopter airframeBoeing Helicopter, together with other United States helicopter manufacturers, participated in a finite element applications program to emplace in the United States a superior capability to utilize finite element analysis models in support of helicopter airframe design. The activities relating to planning and creating a finite element vibrations model of the Boeing Model 36-0 composite airframe are summarized, along with the subsequent analytical correlation with ground shake test data.
Document ID
19890016109
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gabel, R.
(Boeing Helicopter Co. Philadelphia, PA, United States)
Lang, P. F.
(Boeing Helicopter Co. Philadelphia, PA, United States)
Smith, L. A.
(Boeing Helicopter Co. Philadelphia, PA, United States)
Reed, D. A.
(Boeing Helicopter Co. Philadelphia, PA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:181787
NASA-CR-181787
Report Number: NAS 1.26:181787
Report Number: NASA-CR-181787
Accession Number
89N25480
Funding Number(s)
PROJECT: RTOP 505-63-51-01
CONTRACT_GRANT: NAS1-17497
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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