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User's guide for a computer program to analyze the LRC 16 ft transonic dynamics tunnel cable mount systemThe theoretical derivation of the set of equations is discussed which is applicable to modeling the dynamic characteristics of aeroelastically-scaled models flown on the two-cable mount system in a 16 ft transonic dynamics tunnel. The computer program provided for the analysis is also described. The program calculates model trim conditions as well as 3 DOF longitudinal and lateral/directional dynamic conditions for various flying cable and snubber cable configurations. Sample input and output are included.
Document ID
19740002184
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barbero, P. (Grumman Aerospace Corp. Bethpage, NY, United States)
Chin, J. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1973
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-CR-132313
Report Number: NASA-CR-132313
Accession Number
74N10297
Funding Number(s)
CONTRACT_GRANT: NAS1-10635
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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