A new hypersonic boundary layer facility

M. L. Baumgartner; A. J. Smitst; T. Nau; C. W. Rowley

A new hypersonic boundary layer facility

M. L. Baumgartner, A. J. Smitst, T. Nau, C. W. Rowley

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

Abstract

A new Mach 8 blowdown facility for the study of transition, turbulence, and shock wave/boundary layer interactions at high Mach numbers is being built. This paper describes the design and construction of the facility.

Original language	English (US)
State	Published - 1995
Event	33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States Duration: Jan 9 1995 → Jan 12 1995

Other

Other	33rd Aerospace Sciences Meeting and Exhibit, 1995
Country/Territory	United States
City	Reno
Period	1/9/95 → 1/12/95

All Science Journal Classification (ASJC) codes

Space and Planetary Science
Aerospace Engineering

Cite this

@conference{5e14a7902274446dbb21b8ccf1303bac,

title = "A new hypersonic boundary layer facility",

abstract = "A new Mach 8 blowdown facility for the study of transition, turbulence, and shock wave/boundary layer interactions at high Mach numbers is being built. This paper describes the design and construction of the facility.",

author = "Baumgartner, {M. L.} and Smitst, {A. J.} and T. Nau and Rowley, {C. W.}",

note = "Publisher Copyright: {\textcopyright} 1995 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 33rd Aerospace Sciences Meeting and Exhibit, 1995 ; Conference date: 09-01-1995 Through 12-01-1995",

year = "1995",

language = "English (US)",

}

TY - CONF

T1 - A new hypersonic boundary layer facility

AU - Baumgartner, M. L.

AU - Smitst, A. J.

AU - Nau, T.

AU - Rowley, C. W.

PY - 1995

Y1 - 1995

N2 - A new Mach 8 blowdown facility for the study of transition, turbulence, and shock wave/boundary layer interactions at high Mach numbers is being built. This paper describes the design and construction of the facility.

AB - A new Mach 8 blowdown facility for the study of transition, turbulence, and shock wave/boundary layer interactions at high Mach numbers is being built. This paper describes the design and construction of the facility.

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M3 - Paper

AN - SCOPUS:84963533260

T2 - 33rd Aerospace Sciences Meeting and Exhibit, 1995

Y2 - 9 January 1995 through 12 January 1995

ER -

A new hypersonic boundary layer facility

Abstract

Other

All Science Journal Classification (ASJC) codes

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