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Analytical Models for Rotor Test Module, Strut, and Balance Frame Dynamics in the 40 by 80 Ft Wind TunnelA mathematical model is developed for the dynamics of a wind tunnel support system consisting of a balance frame, struts, and an aircraft or test module. Data are given for several rotor test modules in the Ames 40 by 80 ft wind tunnel. A model for ground resonance calculations is also described.
Document ID
19760022180
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johnson, W. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
A-6692
NASA-TM-X-73153
Report Number: A-6692
Report Number: NASA-TM-X-73153
Accession Number
76N29268
Funding Number(s)
PROJECT: RTOP 505-10-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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