Experiments in supersonic turbulent flow with large distributed surface injection

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. https://resolver.caltech.edu/CaltechAUTHORS:20101221-080701462

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Abstract

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.

Item Type:

Article

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

Funders:

Funding Agency	Grant Number
U.S. Army Research Office	UNSPECIFIED
Advanced Research Projects Agency	DA-31-124-ARO(D)-33

Other Numbering System:

Other Numbering System Name	Other Numbering System ID
Guggenheim Jet Propulsion Center	UNSPECIFIED

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Record Number:

CaltechAUTHORS:20101221-080701462

Persistent URL:

https://resolver.caltech.edu/CaltechAUTHORS:20101221-080701462

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

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ID Code:

21462

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CaltechAUTHORS

Deposited By:

Ruth Sustaita

Deposited On:

05 Jan 2011 22:17

Last Modified:

03 Oct 2019 02:24

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