Control of a supersonic reattaching shear layer

J. Poggie; A. J. Smits

Control of a supersonic reattaching shear layer

J. Poggie, A. J. Smits

Mechanical & Aerospace Engineering

Research output: Contribution to conference › Paper › peer-review

Abstract

A reattaching supersonic shear layer was perturbed by transverse air injection, and the effects were investigated using flow visualization. It was found that shear layer mixing was increased and that the shock system was strongly disturbed due to the heightened three dimensionality of the flow. Mixing enhancement was also achieved in an incompressible downstream-facing step flow using the same blowing procedure.

Original language	English (US)
State	Published - 1993
Event	AIAA 2nd Shear Flow Conference, 1993 - Orlando, United States Duration: Jul 6 1993 → Jul 9 1993

Other

Other	AIAA 2nd Shear Flow Conference, 1993
Country/Territory	United States
City	Orlando
Period	7/6/93 → 7/9/93

All Science Journal Classification (ASJC) codes

General Engineering

Cite this

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title = "Control of a supersonic reattaching shear layer",

abstract = "A reattaching supersonic shear layer was perturbed by transverse air injection, and the effects were investigated using flow visualization. It was found that shear layer mixing was increased and that the shock system was strongly disturbed due to the heightened three dimensionality of the flow. Mixing enhancement was also achieved in an incompressible downstream-facing step flow using the same blowing procedure.",

author = "J. Poggie and Smits, {A. J.}",

note = "Publisher Copyright: {\textcopyright} 1993 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; AIAA 2nd Shear Flow Conference, 1993 ; Conference date: 06-07-1993 Through 09-07-1993",

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TY - CONF

T1 - Control of a supersonic reattaching shear layer

AU - Poggie, J.

AU - Smits, A. J.

PY - 1993

Y1 - 1993

N2 - A reattaching supersonic shear layer was perturbed by transverse air injection, and the effects were investigated using flow visualization. It was found that shear layer mixing was increased and that the shock system was strongly disturbed due to the heightened three dimensionality of the flow. Mixing enhancement was also achieved in an incompressible downstream-facing step flow using the same blowing procedure.

AB - A reattaching supersonic shear layer was perturbed by transverse air injection, and the effects were investigated using flow visualization. It was found that shear layer mixing was increased and that the shock system was strongly disturbed due to the heightened three dimensionality of the flow. Mixing enhancement was also achieved in an incompressible downstream-facing step flow using the same blowing procedure.

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UR - http://www.scopus.com/inward/citedby.url?scp=84990886688&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:84990886688

T2 - AIAA 2nd Shear Flow Conference, 1993

Y2 - 6 July 1993 through 9 July 1993

ER -

Control of a supersonic reattaching shear layer

Abstract

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All Science Journal Classification (ASJC) codes

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