A combined experimental and numerical study of a three-dimensional supersonic turbulent boundary layer

W. Konrad; A. J. Smits; D. Knight

doi:10.1016/0894-1777(94)90108-2

A combined experimental and numerical study of a three-dimensional supersonic turbulent boundary layer

W. Konrad, A. J. Smits, D. Knight

Mechanical & Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

8 Scopus citations

Abstract

Experimental and numerical mean data are compared in detail for a three-dimensional supersonic turbulent boundary layer generated by an isentropic compression. Three distinct flow regimes were identified in the mean flow field. Turbulence intensities measured in the three-dimensional flow are compared to corresponding two-dimensional adverse pressure gradient flows to determine the effects of three-dimensionality.

Original language	English (US)
Pages (from-to)	156-164
Number of pages	9
Journal	Experimental Thermal and Fluid Science
Volume	9
Issue number	2
DOIs	https://doi.org/10.1016/0894-1777(94)90108-2
State	Published - Aug 1994

All Science Journal Classification (ASJC) codes

Chemical Engineering(all)
Nuclear Energy and Engineering
Aerospace Engineering
Mechanical Engineering
Fluid Flow and Transfer Processes

Keywords

isentropic compression
supersonic flow
three-dimensional flow
turbulent boundary layer

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10.1016/0894-1777(94)90108-2

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title = "A combined experimental and numerical study of a three-dimensional supersonic turbulent boundary layer",

abstract = "Experimental and numerical mean data are compared in detail for a three-dimensional supersonic turbulent boundary layer generated by an isentropic compression. Three distinct flow regimes were identified in the mean flow field. Turbulence intensities measured in the three-dimensional flow are compared to corresponding two-dimensional adverse pressure gradient flows to determine the effects of three-dimensionality.",

keywords = "isentropic compression, supersonic flow, three-dimensional flow, turbulent boundary layer",

author = "W. Konrad and Smits, {A. J.} and D. Knight",

note = "Funding Information: This research was sponsored by the Air Force Office of Scientific Research under AFOSR grants 89-0033 and 86-0266 monitored by Dr. Len Sakeli. Supercomputer resources were provided by NASA Ames Research Center. Analysis of the flow field was performed at the College of Engineering Supercomputer Remote Access Facility sponsored by Rutgers University. Analysis of the flow-field structure was performed at and sponsored by Princeton University.",

year = "1994",

month = aug,

doi = "10.1016/0894-1777(94)90108-2",

language = "English (US)",

volume = "9",

pages = "156--164",

journal = "Experimental Thermal and Fluid Science",

issn = "0894-1777",

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T1 - A combined experimental and numerical study of a three-dimensional supersonic turbulent boundary layer

AU - Konrad, W.

AU - Smits, A. J.

AU - Knight, D.

N1 - Funding Information: This research was sponsored by the Air Force Office of Scientific Research under AFOSR grants 89-0033 and 86-0266 monitored by Dr. Len Sakeli. Supercomputer resources were provided by NASA Ames Research Center. Analysis of the flow field was performed at the College of Engineering Supercomputer Remote Access Facility sponsored by Rutgers University. Analysis of the flow-field structure was performed at and sponsored by Princeton University.

PY - 1994/8

Y1 - 1994/8

N2 - Experimental and numerical mean data are compared in detail for a three-dimensional supersonic turbulent boundary layer generated by an isentropic compression. Three distinct flow regimes were identified in the mean flow field. Turbulence intensities measured in the three-dimensional flow are compared to corresponding two-dimensional adverse pressure gradient flows to determine the effects of three-dimensionality.

AB - Experimental and numerical mean data are compared in detail for a three-dimensional supersonic turbulent boundary layer generated by an isentropic compression. Three distinct flow regimes were identified in the mean flow field. Turbulence intensities measured in the three-dimensional flow are compared to corresponding two-dimensional adverse pressure gradient flows to determine the effects of three-dimensionality.

KW - isentropic compression

KW - supersonic flow

KW - three-dimensional flow

KW - turbulent boundary layer

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SN - 0894-1777

VL - 9

SP - 156

EP - 164

JO - Experimental Thermal and Fluid Science

JF - Experimental Thermal and Fluid Science

IS - 2

ER -

A combined experimental and numerical study of a three-dimensional supersonic turbulent boundary layer

Abstract

All Science Journal Classification (ASJC) codes

Keywords

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