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Design study of advanced model support systems for the National Transonic Facility (NTF)It has long been recognized that the sting (or support system) is a very critical part of the model system. The designer is frequently faced with the tradeoff of minimizing sting size, thereby compromising facility and model safety, against a larger sting and the subsequent problems of sting interference effects. In the NASA Langley Research Center National Transonic Facility (NTF), this problem is accentuated by the severe environment of high pressure/low temperature, designed into the facility to provide the desired high Reynolds number. Compromises in the configuration geometry and/or limiting the test envelope are therefore contrary to the purposes and goals of the NTF and are unacceptable. The results of an investigation aimed at improvements of 25% in both strength and Young's modulus of elasticity as compared to high strength cryogenically acceptable steels currently being used are presented. Various materials or combinations of materials were studied along with different design approaches. Design concepts were developed which included conventional material stings, advanced composites, and hybrid configurations. Candidate configurations are recommended.
Document ID
19870010864
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:178214
NASA-CR-178214
Accession Number
87N20297
Funding Number(s)
PROJECT: RTOP 505-61-01-07
CONTRACT_GRANT: NASA ORDER L-997258
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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