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Experimental studies on the aerodynamic performance and dynamic response of flow direction sensing vanesSystematic investigations were performed on a variety of aerodynamic surfaces to obtain their potential for possible application to wind vanes. Among the surfaces tested were: (1) single vanes consisting of flat plates of various planforms having aspect ratios between 0.5 and 5; (2) bi-vanes with aspect ratio 2.5; (3) various cone and box vanes; and (4) various cruciform configurations. The models were subjected to windtunnel tests. In addition to lift and drag force measurements, damping and frequency test were performed under a variety of flow conditions.
Document ID
19760017144
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barna, P. S.
(Old Dominion Univ. Norfolk, VA, United States)
Crossman, G. R.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1976
Publication Information
Publisher: NASA
Subject Category
Aircraft Instrumentation
Report/Patent Number
REPT-75-T7
NASA-CR-2683
Accession Number
76N24232
Funding Number(s)
CONTRACT_GRANT: NSG-1143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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