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Rotary mechanism for wind tunnel stall/spin studiesThe critical problem of stall-spin characteristics of high performance aircraft and the need for experimental data in this area are reviewed. A rotary mechanism for obtaining this aerodynamic data in a conventional wind tunnel is presented. The intricacies of the drive systems and the articulation available through such a mechanism are described.
Document ID
19760021190
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mancini, R. E. (NASA Ames Research Center Moffett Field, CA, United States)
Matsuhiro, D. S. (NASA Ames Research Center Moffett Field, CA, United States)
Vallotton, W. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Research And Support Facilities (Air)
Accession Number
76N28278
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760021184Collected WorksTenth Aerospace Mechanisms Symposium
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