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Ground shake test of the UH-60A helicopter airframe and comparison with NASTRAN finite element model predictionsSikorsky Aircraft, together with the other major helicopter airframe manufacturers, is engaged in a study to improve the use of finite element analysis to predict the dynamic behavior of helicopter airframes, under a rotorcraft structural dynamics program called DAMVIBS (Design Analysis Methods for VIBrationS), sponsored by the NASA-Langley. The test plan and test results are presented for a shake test of the UH-60A BLACK HAWK helicopter. A comparison is also presented of test results with results obtained from analysis using a NASTRAN finite element model.
Document ID
19900015827
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Howland, G. R.
(Sikorsky Aircraft Stratford, CT, United States)
Durno, J. A.
(Sikorsky Aircraft Stratford, CT, United States)
Twomey, W. J.
(Sikorsky Aircraft Stratford, CT, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-181993
NAS 1.26:181993
Report Number: NASA-CR-181993
Report Number: NAS 1.26:181993
Accession Number
90N25143
Funding Number(s)
PROJECT: RTOP 505-63-51-01
CONTRACT_GRANT: NAS1-17499
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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