Frenandez, F. L. and Zukoski, E. E. (1969) Experiments in supersonic turbulent flow with large distributed surface injection. AIAA Journal, 7 (9). pp. 1759-1767. ISSN 0001-1452 http://resolver.caltech.edu/CaltechAUTHORS:20101221-080701462
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The mean velocity and pressure fields in a turbulent boundary layer on a Hat plate at M∞ = 2.6 are investigated for ratios of mass-How per unit area injected at the wall to that at the edge of the boundary layer (Λ_e) between 0 and 0.03. Two-dimensionality is demonstrated, and a similar How approached with linear growth of momentum and displacement thicknesses. A Howarth-Dorodnitsyn transformation for the normal coordinate is found to bring the data into good agreement with incompressible results for the same value of Λ_e. At the highest injection rate, the transformed velocity profiles agree well with incompressible turbulent mixing layer results. Finally, the induced side forces are found to be comparable to those obtained by equivalent injection through a slot.
|Additional Information:||© 1969, by the American Institute of Aeronautics and Astronautics. Reprinted from AIAA JOURNAL, Vol. 7, No.9, September 1969, pp. 1759-1767. Presented as Paper 68-129 at the AIAA 6th Aerospace Sciences Meeting, New York, January 22-24,1968; submitted September 23, 1968; revision received February 24, 1969. This work was supported by the U.S. Army Research Office and the Advanced Research Projects Agency, Contract DA-31-124-ARO(D)-33.|
|Group:||Guggenheim Jet Propulsion Center|
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|Official Citation:||Experiments in supersonic turbulent flow with large distributed surface injection. FERNANDEZ, F. L. /AEROSPACE CORP., FLUID MECHANICS DEPT., SAN BERNARDINO, CALIF./;ZUKOSKI, E. E. /CALIFORNIA INST. OF TECH., DANIEL AND FLORENCE GUGGENHEIM JET PROPULSION CENTER, PASADENA, CALIF. AIAA Journal (0001-1452) 1969 vol. 7 no. 9|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||05 Jan 2011 22:17|
|Last Modified:||26 Dec 2012 12:47|
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