Fernandez, F. L. and Zukoski, E. E. (1968) Experiments in supersonic turbulent flow with large distributed surface injection. AIAA Papers, 68-129. California Institute of Technology , Pasadena, CA. http://resolver.caltech.edu/CaltechAUTHORS:20101223-075127801
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The mean velocity and pressure fields in a turbulent boundary layer on a flat plate at M_∞ = 2.6 are investigated for ratios of mass flow 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 flow established 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 velocity profiles agree well with turbulent mixing-layer results. However, unlike mixing layers, the maximum rate of mass entrainment is the same as for the incompressible case. Finally,the induced side forces are found to be comparable to those obtained by equivalent inje ction thr ough a slot.
|Item Type:||Report or Paper (Report)|
|Additional Information:||© 1968, American Institute of Aeronautics and Astronautics. This work was supported by the U. S. Army Research Office and the Advanced Research Projects Agency, Contract No. DA-31-l24-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-1968-129 AMERICAN INST OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 6TH, NEW YORK, N.Y., Jan 22-24, 1968. AIAA JOURNAL|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||05 Jan 2011 22:16|
|Last Modified:||26 Dec 2012 12:47|
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