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A device for introducing helical perturbations into a trailing line vortexA perturbation generator has been designed which can be attached to the centerbody of a matched airfoil type vortex generator. The device was desired to enable the introduction of helical-wave, velocity perturbations into a vortex core to permit experimental verification of theoretical vortex stability predictions. Evaluation of the perturbation generator performance, prior to vortex stability studies, has been reported here. Controlled perturbations with frequencies above 200 hz have been produced, but visual observations were insufficient to confirm their helical character. Hot wire velocity spectrum data have confirmed the device's ability to introduce controlled frequency fluctuations. In addition, other flow oscillations have been discussed which can influence the controllability of vortex perturbations.
Document ID
19900051701
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ash, Robert L.
(Old Dominion University Norfolk, VA, United States)
Riester, John E., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
June 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-1627
Report Number: AIAA PAPER 90-1627
Accession Number
90A38756
Funding Number(s)
CONTRACT_GRANT: NAS1-18599
CONTRACT_GRANT: NAG1-530
Distribution Limits
Public
Copyright
Other

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