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Wake profile measurements of fixed and oscillating flapsAlthough the potential of laser velocimetry for the non-intrusive measurement of complex shear flows has long been recognized, there have been few applications in other small, closely controlled laboratory situations. Measurements in large scale, high speed wind tunnels are still a complex task. To support a study of periodic flows produced by an oscillating edge flap in the Ames eleven foot wind tunnel, this study was done. The potential for laser velocimeter measurements in large scale production facilities are evaluated. The results with hot wire flow field measurements are compared.
Document ID
19840026357
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Owen, F. K.
(Compass Systems, Inc. San Diego, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:166602
NASA-CR-166602
Report Number: NAS 1.26:166602
Report Number: NASA-CR-166602
Accession Number
84N34428
Funding Number(s)
CONTRACT_GRANT: NAS2-11080
PROJECT: RTOP 505-31-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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