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Application of laser velocimetry to aircraft wake-vortex measurementsThe theory and use of a laser velocimeter that makes simultaneous measurements of vertical and longitudinal velocities while rapidly scanning a flow field laterally are described, and its direct application to trailing wake-vortex research is discussed. Pertinent measurements of aircraft wake-vortex velocity distributions obtained in a wind tunnel and water towing tank are presented. The utility of the velocimeter to quantitatively assess differences in wake velocity distributions due to wake dissipating devices and span loading changes on the wake-generating model is also demonstrated.
Document ID
19780004078
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ciffone, D. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Orloff, K. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Publication Information
Publication: Wake Vortex Minimization
Subject Category
Aerodynamics
Accession Number
78N12021
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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