Structure of a mach 8 turbulent boundary layer

Mark L. Baurngartner; Peter J. Erbland; Michael R. Etz; Azer Yalin; Brian K. Muzas; Alexander J. Smits; Walter R. Lempert; Richard B. Miles

Structure of a mach 8 turbulent boundary layer

Mark L. Baurngartner, Peter J. Erbland, Michael R. Etz, Azer Yalin, Brian K. Muzas, Alexander J. Smits, Walter R. Lempert, Richard B. Miles

Mechanical & Aerospace Engineering

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

10 Scopus citations

Abstract

Preliminary measurements of the effects of increasing Mach number on the structure of turbulent boundary layers are presented. The data were obtained using a Mach 2.5 pilot tunnel facility and a new Mach 8 boundary layer facility. The principal diagnostic technique was planar Rayleigh scattering. The results shed some light on the effects of Mach and Reynolds number on outer layer intermittency.

Original language	English (US)
State	Published - 1997
Event	35th Aerospace Sciences Meeting and Exhibit, 1997 - Reno, United States Duration: Jan 6 1997 → Jan 9 1997

Other

Other	35th Aerospace Sciences Meeting and Exhibit, 1997
Country/Territory	United States
City	Reno
Period	1/6/97 → 1/9/97

All Science Journal Classification (ASJC) codes

Space and Planetary Science
Aerospace Engineering

Cite this

@conference{508d5a707e2f45e7a9bea815e4530922,

title = "Structure of a mach 8 turbulent boundary layer",

abstract = "Preliminary measurements of the effects of increasing Mach number on the structure of turbulent boundary layers are presented. The data were obtained using a Mach 2.5 pilot tunnel facility and a new Mach 8 boundary layer facility. The principal diagnostic technique was planar Rayleigh scattering. The results shed some light on the effects of Mach and Reynolds number on outer layer intermittency.",

author = "Baurngartner, {Mark L.} and Erbland, {Peter J.} and Etz, {Michael R.} and Azer Yalin and Muzas, {Brian K.} and Smits, {Alexander J.} and Lempert, {Walter R.} and Miles, {Richard B.}",

note = "Publisher Copyright: {\textcopyright} 1997 American Institute of Aeronautics and Astronautics, Inc.; 35th Aerospace Sciences Meeting and Exhibit, 1997 ; Conference date: 06-01-1997 Through 09-01-1997",

year = "1997",

language = "English (US)",

}

TY - CONF

T1 - Structure of a mach 8 turbulent boundary layer

AU - Baurngartner, Mark L.

AU - Erbland, Peter J.

AU - Etz, Michael R.

AU - Yalin, Azer

AU - Muzas, Brian K.

AU - Smits, Alexander J.

AU - Lempert, Walter R.

AU - Miles, Richard B.

PY - 1997

Y1 - 1997

N2 - Preliminary measurements of the effects of increasing Mach number on the structure of turbulent boundary layers are presented. The data were obtained using a Mach 2.5 pilot tunnel facility and a new Mach 8 boundary layer facility. The principal diagnostic technique was planar Rayleigh scattering. The results shed some light on the effects of Mach and Reynolds number on outer layer intermittency.

AB - Preliminary measurements of the effects of increasing Mach number on the structure of turbulent boundary layers are presented. The data were obtained using a Mach 2.5 pilot tunnel facility and a new Mach 8 boundary layer facility. The principal diagnostic technique was planar Rayleigh scattering. The results shed some light on the effects of Mach and Reynolds number on outer layer intermittency.

UR - http://www.scopus.com/inward/record.url?scp=84983210820&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84983210820&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:84983210820

T2 - 35th Aerospace Sciences Meeting and Exhibit, 1997

Y2 - 6 January 1997 through 9 January 1997

ER -

Structure of a mach 8 turbulent boundary layer

Abstract

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All Science Journal Classification (ASJC) codes

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