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Shear layer excitation, experiment versus theoryThe acoustical excitation of shear layers is investigated. Acoustical excitation causes the so-called orderly structures in shear layers and jets. Also, the deviations in the spreading rate between different shear layer experiments are due to the same excitation mechanism. Measurements in the linear interaction region close to the edge from which the shear layer is shed are examined. Two sets of experiments (Houston 1981 and Berlin 1983/84) are discussed. The measurements were carried out with shear layers in air using hot wire anemometers and microphones. The agreement between these measurements and the theory is good. Even details of the fluctuating flow field correspond to theoretical predictions, such as the local occurrence of negative phase speeds.
Document ID
19860011251
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bechert, D. W.
(Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt Goettingen, Germany)
Stahl, B.
(Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt Goettingen, Germany)
Date Acquired
September 5, 2013
Publication Date
January 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-176604
NAS 1.26:176604
DFVLR-FB-84-26
Report Number: NASA-CR-176604
Report Number: NAS 1.26:176604
Report Number: DFVLR-FB-84-26
Accession Number
86N20722
Funding Number(s)
CONTRACT_GRANT: NAG3-198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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