BEHAVIOUR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER UNDER INCIPIENT SEPARATION CONDITIONS.

K. C. Muck; A. J. Smits

doi:10.1007/978-3-642-69996-2_19

BEHAVIOUR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER UNDER INCIPIENT SEPARATION CONDITIONS.

K. C. Muck
, A. J. Smits

Mechanical & Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

4 Scopus citations

Abstract

This paper presents an experimental study of a turbulent boundary-layer/shock-wave interaction. The interaction was generated by a two-dimensional compression corner, and the flow was on the point of separating. Measurements were made using both normal and inclined hot wires, and the data include measurements of the longitudinal mass-flow fluctuation intensity and the mass-weighted Reynolds shear stress. Refs.

Original language	English (US)
Title of host publication	Unknown Host Publication Title
Publisher	Springer Verlag
Pages	235-245
Number of pages	11
ISBN (Print)	3540137440, 9783540137443
DOIs	https://doi.org/10.1007/978-3-642-69996-2_19
State	Published - 1985

All Science Journal Classification (ASJC) codes

General Engineering

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10.1007/978-3-642-69996-2_19

Cite this

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title = "BEHAVIOUR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER UNDER INCIPIENT SEPARATION CONDITIONS.",

abstract = "This paper presents an experimental study of a turbulent boundary-layer/shock-wave interaction. The interaction was generated by a two-dimensional compression corner, and the flow was on the point of separating. Measurements were made using both normal and inclined hot wires, and the data include measurements of the longitudinal mass-flow fluctuation intensity and the mass-weighted Reynolds shear stress. Refs.",

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Y1 - 1985

N2 - This paper presents an experimental study of a turbulent boundary-layer/shock-wave interaction. The interaction was generated by a two-dimensional compression corner, and the flow was on the point of separating. Measurements were made using both normal and inclined hot wires, and the data include measurements of the longitudinal mass-flow fluctuation intensity and the mass-weighted Reynolds shear stress. Refs.

AB - This paper presents an experimental study of a turbulent boundary-layer/shock-wave interaction. The interaction was generated by a two-dimensional compression corner, and the flow was on the point of separating. Measurements were made using both normal and inclined hot wires, and the data include measurements of the longitudinal mass-flow fluctuation intensity and the mass-weighted Reynolds shear stress. Refs.

UR - https://www.scopus.com/pages/publications/0021945043

UR - https://www.scopus.com/pages/publications/0021945043#tab=citedBy

U2 - 10.1007/978-3-642-69996-2_19

DO - 10.1007/978-3-642-69996-2_19

M3 - Conference contribution

AN - SCOPUS:0021945043

SN - 3540137440

SN - 9783540137443

SP - 235

EP - 245

BT - Unknown Host Publication Title

PB - Springer Verlag

ER -

BEHAVIOUR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER UNDER INCIPIENT SEPARATION CONDITIONS.

Abstract

All Science Journal Classification (ASJC) codes

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