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Simple theoretical models for composite rotor bladesThe development of theoretical rotor blade structural models for designs based upon composite construction is discussed. Care was exercised to include a member of nonclassical effects that previous experience indicated would be potentially important to account for. A model, representative of the size of a main rotor blade, is analyzed in order to assess the importance of various influences. The findings of this model study suggest that for the slenderness and closed cell construction considered, the refinements are of little importance and a classical type theory is adequate. The potential of elastic tailoring is dramatically demonstrated, so the generality of arbitrary ply layup in the cell wall is needed to exploit this opportunity.
Document ID
19850014071
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Valisetty, R. R.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Rehfield, L. W.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:175620
NASA-CR-175620
Accession Number
85N22382
Funding Number(s)
CONTRACT_GRANT: NAG1-398
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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