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Program user's manual for an unsteady helicopter rotor-fuselage aerodynamic analysisThe Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter rotor and fuselage. This manual describes the structure and operation of the computer programs that make up the Rotor-Fuselage Analysis, programs which prepare the input and programs which display the output.
Document ID
19880018663
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lorber, Peter F.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
UTRC/R88-956977
NASA-CR-181701
NAS 1.26:181701
Report Number: UTRC/R88-956977
Report Number: NASA-CR-181701
Report Number: NAS 1.26:181701
Accession Number
88N28047
Funding Number(s)
CONTRACT_GRANT: NAS1-17469
PROJECT: RTOP 505-61-51-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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