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User's guide for a revised computer program to analyze the LRC 16 foot transonic dynamics tunnel active cable mount systemThe revision of an existing digital program to analyze the stability of models mounted on a two-cable mount system used in a transonic dynamics wind tunnel is presented. The program revisions and analysis of an active feedback control system to be used for controlling the free-flying models are treated.
Document ID
19750021057
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chin, J. (Grumman Aerospace Corp. Bethpage, NY, United States)
Barbero, P. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-132692
Report Number: NASA-CR-132692
Accession Number
75N29130
Funding Number(s)
CONTRACT_GRANT: NAS1-10635
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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