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A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 2: User's manualThe use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dynamics is described. The program calculates the loads and motion of helicopter rotors and airframe. First the trim solution is obtained, then the flutter, flight dynamics, and/or transient behavior can be calculated. Either a new job can be initiated or further calculations can be performed for an old job.
Document ID
19800019796
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johnson, W. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TM-81183
AVRADCOM-TR-80-A-6-PT-2
A-8101
Report Number: NASA-TM-81183
Report Number: AVRADCOM-TR-80-A-6-PT-2
Report Number: A-8101
Accession Number
80N28297
Funding Number(s)
PROJECT: RTOP 505-42-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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