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Research program to determine rotor response characteristics at high advance ratios Final reportStability and response characteristics of directly controlled rigid rotors at high advance ratios and correlation of mathematical model with wind tunnel test data
Document ID
19710010946
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuczynski, W. A.
(Lockheed-California Co. Burbank, CA, United States)
Sissingh, G. J.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Subject Category
Aircraft
Report/Patent Number
LR-24122
NASA-CR-114290
Report Number: LR-24122
Report Number: NASA-CR-114290
Accession Number
71N20421
Funding Number(s)
CONTRACT_GRANT: NAS2-5419
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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