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Transonic, turbulent boundary-layer separation generated on an axisymmetric flow modelExperimental data describing the transonic, turbulent, separated flow generated by an axisymmetric flow model are presented. The model consisted of a circular-arc bump affixed to a straight, circular cylinder aligned with the flow direction. Measurements of the mean velocity, turbulence intensity, and Reynolds shear-stress profiles were made in the separated flow. These data revealed dramatic changes in the shear-stress levels as the flow passed through the interaction to reattachment. Behavior of the turbulence reaction to the imposed pressure gradients was examined in terms of the mixing length and the excursions of the turbulence from equilibrium.
Document ID
19860043801
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bachalo, W. D.
(Aerometrics, Inc. Mountain View, CA, United States)
Johnson, D. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1986
Publication Information
Publication: AIAA Journal
Volume: 24
ISSN: 0001-1452
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0001-1452
Accession Number
86A28539
Distribution Limits
Public
Copyright
Other

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