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Elastic suspension of a wind tunnel test sectionExperimental verification of the theory describing arbitrary motions of an airfoil is reported. The experimental apparatus is described. A mechanism was designed to provide two separate degrees of freedom without friction or backlash to mask the small but important aerodynamic effects of interest.
Document ID
19820015489
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hacker, R. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Rock, S. (Systems Control Inc. Palo Alto, Calif., United States)
Debra, D. B. (Sanford Univ.)
Date Acquired
August 10, 2013
Publication Date
May 1, 1982
Publication Information
Publication: NASA. Kennedy Space Center The 16th Aerospace Mech. Symp.
Subject Category
Research And Support Facilities (Air)
Accession Number
82N23363
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820015470Collected WorksThe 16th Aerospace Mechanisms Symposium
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