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Visualization of quasi-periodic unsteady flowsA self-synchronizing schlieren flow visualization technique has been developed to study unsteady periodic flows which may result from aeroelastic effects. The technique allows the experimentalist to stroboscopically 'freeze' the streak line pattern at any phase in one period of the motion by driving the schlieren light source with an electronically processed synchronizing signal that is derived by measuring a periodic flow variable with a convenient sensor. Results for the visualization of the near-wake behind an oscillating airfoil at low speeds which show an ordered series of discrete vortices and a curious short-wave-length wake disturbance are examined. Results are also presented for edge tone sound generation.
Document ID
19780045895
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Kadlec, R. A.
(Colorado, University Boulder, Colo., United States)
Davis, S. S.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 78-502
Report Number: AIAA PAPER 78-502
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Bethesda, MD
Start Date: April 3, 1978
End Date: April 5, 1978
Accession Number
78A29804
Distribution Limits
Public
Copyright
Other

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