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Features of a separating turbulent boundary layer in the vicinity of separationLaser anemometer measurements using a directionally sensitive system were obtained for a nominally two-dimensional separating turbulent boundary layer produced by an adverse pressure gradient. An airfoil-type flow was generated in which the flow was accelerated and then decelerated until separation. The results include the skin friction, mean velocity profiles, turbulent shear stresses and intensities, spectra, dissipation rate, turbulent/non-turbulent interfacial intermittency, and eddy speeds.
Document ID
19770044401
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Simpson, R. L.
(Southern Methodist Univ. Dallas, TX, United States)
Strickland, J. H.
(Southern Methodist Univ. Dallas, TX, United States)
Barr, P. W.
(Southern Methodist University Dallas, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
March 9, 1977
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 79
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
77A27253
Funding Number(s)
CONTRACT_GRANT: NGL-44-007-006
CONTRACT_GRANT: DA-ARO(D)-31-124-72-G31
CONTRACT_GRANT: DAHC04-74-G-0024
Distribution Limits
Public
Copyright
Other

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