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NASA Glenn Wind Tunnel Model Systems CriteriaThis report describes criteria for the design, analysis, quality assurance, and documentation of models that are to be tested in the wind tunnel facilities at the NASA Glenn Research Center. This report presents two methods for computing model allowable stresses on the basis of the yield stress or ultimate stress, and it defines project procedures to test models in the NASA Glenn aeropropulsion facilities. Both customer-furnished and in-house model systems are discussed. The functions of the facility personnel and customers are defined. The format for the pretest meetings, safety permit process, and model reviews are outlined. The format for the model systems report (a requirement for each model that is to be tested at NASA Glenn) is described, the engineers responsible for developing the model systems report are listed, and the timetable for its delivery to the project engineer is given.
Document ID
20040082333
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Soeder, Ronald H.
(NASA Glenn Research Center Cleveland, OH, United States)
Roeder, James W.
(NASA Glenn Research Center Cleveland, OH, United States)
Stark, David E.
(NASA Glenn Research Center Cleveland, OH, United States)
Linne, Alan A.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2004-212706/REV1
E-14216-1-REV1
Report Number: NASA/TM-2004-212706/REV1
Report Number: E-14216-1-REV1
Funding Number(s)
WBS: WBS 22-708-90-63
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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