The effects of streamline curvature and pressure gradient on the behavior of turbulent boundary layers in supersonic flow

Douglas R. Smith; Alexander J. Smits

The effects of streamline curvature and pressure gradient on the behavior of turbulent boundary layers in supersonic flow

Douglas R. Smith, Alexander J. Smits

Mechanical & Aerospace Engineering

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

10 Scopus citations

Abstract

Turbulence measurements in distorted supersonic flows are reviewed in the interest of elucidating the effects of curvature, pressure gradients and shockwaves on the boundary layer turbulence structure.

Original language	English (US)
State	Published - 1994
Event	AIAA Fluid Dynamics Conference, 1994 - Colorado Springs, United States Duration: Jun 20 1994 → Jun 23 1994

Other

Other	AIAA Fluid Dynamics Conference, 1994
Country/Territory	United States
City	Colorado Springs
Period	6/20/94 → 6/23/94

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Engineering (miscellaneous)

Cite this

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title = "The effects of streamline curvature and pressure gradient on the behavior of turbulent boundary layers in supersonic flow",

abstract = "Turbulence measurements in distorted supersonic flows are reviewed in the interest of elucidating the effects of curvature, pressure gradients and shockwaves on the boundary layer turbulence structure.",

author = "Smith, \{Douglas R.\} and Smits, \{Alexander J.\}",

note = "Publisher Copyright: {\textcopyright} 1994 by D.R. Smith. Published by the AIAA, Inc. with permission.; AIAA Fluid Dynamics Conference, 1994 ; Conference date: 20-06-1994 Through 23-06-1994",

year = "1994",

language = "English (US)",

}

TY - CONF

T1 - The effects of streamline curvature and pressure gradient on the behavior of turbulent boundary layers in supersonic flow

AU - Smith, Douglas R.

AU - Smits, Alexander J.

PY - 1994

Y1 - 1994

N2 - Turbulence measurements in distorted supersonic flows are reviewed in the interest of elucidating the effects of curvature, pressure gradients and shockwaves on the boundary layer turbulence structure.

AB - Turbulence measurements in distorted supersonic flows are reviewed in the interest of elucidating the effects of curvature, pressure gradients and shockwaves on the boundary layer turbulence structure.

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M3 - Paper

AN - SCOPUS:84997822667

T2 - AIAA Fluid Dynamics Conference, 1994

Y2 - 20 June 1994 through 23 June 1994

ER -

The effects of streamline curvature and pressure gradient on the behavior of turbulent boundary layers in supersonic flow

Abstract

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All Science Journal Classification (ASJC) codes

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