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On the structure of hypersonic turbulent boundary layers.Extensive hot-wire auto- and cross-correlation measurements obtained in a fully developed compressible turbulent boundary layer are presented. A tentative mechanism of turbulence production and growth in hypersonic flow suggested by these measurements is developed. This flow model is consistent with previous observations in incompressible flows. Detailed measurements of the mean properties of the hypersonic turbulent boundary layer are also presented and compared with results from various transformation and finite-difference prediction methods. It is shown that none of the theories predict all the properties of the hypersonic turbulent boundary layer and that additional measurements are needed to provide more adequate physics of turbulent processes for use in the various theories.
Document ID
19720051522
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Owen, F. K.
Horstman, C. C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
June 27, 1972
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 53
Subject Category
Fluid Mechanics
Accession Number
72A35188
Distribution Limits
Public
Copyright
Other

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