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Simplified procedures for estimating flapwise bending moments on helicopter rotor blades. Part 2 - TablesTabulated bending moment transfer coefficients for helicopter rotor blades
Document ID
19690030970
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Landgrebe, A. J. (United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-1441
Report Number: NASA-CR-1441
Accession Number
69N40359
Funding Number(s)
CONTRACT_GRANT: NAS1-7880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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