Rayleigh imaging and flow tagging in ground test facilities

R Miles; W.  Lempert; B. Zhang; J Forkey; Ivan Glesk

doi:10.1109/ICIASF.1991.186247

Rayleigh imaging and flow tagging in ground test facilities

R Miles, W. Lempert, B. Zhang, J Forkey, Ivan Glesk

Electronic And Electrical Engineering

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

2 Citations (Scopus)

Abstract

The authors present preliminary results on the application of ultraviolet Rayleigh imaging and RELIEF flow tagging to a high Reynolds number, Mach 3 blow-down air facility at Princeton University's Gas Dynamics Laboratory. RELIEF tagging was accomplished using stimulated Raman scattering to vibrationally excited oxygen molecules. Examples include instantaneous images of boundary-layer structure and shock-wave/boundary-layer interactions, as well as results of flow tagging velocity measurements in the free-stream and boundary-layer regions of this facility. The future implementation of filtered Rayleigh scattering is also discussed.

Original language	English
Title of host publication	International Congress on Instrumentation in Aerospace Simulation Facilities, 1991
Subtitle of host publication	ICIASF '91 Record
Place of Publication	Piscataway, NJ, United States
Publisher	IEEE
Pages	255-261
Number of pages	7
DOIs	https://doi.org/10.1109/ICIASF.1991.186247
Publication status	Published - 27 Oct 1991

Keywords

filtered Rayleigh scattering
RELIEF flow tagging
Mach 3 blow-down air facility
stimulated Raman scattering
flow tagging

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10.1109/ICIASF.1991.186247

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title = "Rayleigh imaging and flow tagging in ground test facilities",

abstract = "The authors present preliminary results on the application of ultraviolet Rayleigh imaging and RELIEF flow tagging to a high Reynolds number, Mach 3 blow-down air facility at Princeton University's Gas Dynamics Laboratory. RELIEF tagging was accomplished using stimulated Raman scattering to vibrationally excited oxygen molecules. Examples include instantaneous images of boundary-layer structure and shock-wave/boundary-layer interactions, as well as results of flow tagging velocity measurements in the free-stream and boundary-layer regions of this facility. The future implementation of filtered Rayleigh scattering is also discussed.",

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author = "R Miles and W. Lempert and B. Zhang and J Forkey and Ivan Glesk",

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language = "English",

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AU - Miles, R

AU - Lempert, W.

AU - Zhang, B.

AU - Forkey, J

AU - Glesk, Ivan

PY - 1991/10/27

Y1 - 1991/10/27

N2 - The authors present preliminary results on the application of ultraviolet Rayleigh imaging and RELIEF flow tagging to a high Reynolds number, Mach 3 blow-down air facility at Princeton University's Gas Dynamics Laboratory. RELIEF tagging was accomplished using stimulated Raman scattering to vibrationally excited oxygen molecules. Examples include instantaneous images of boundary-layer structure and shock-wave/boundary-layer interactions, as well as results of flow tagging velocity measurements in the free-stream and boundary-layer regions of this facility. The future implementation of filtered Rayleigh scattering is also discussed.

AB - The authors present preliminary results on the application of ultraviolet Rayleigh imaging and RELIEF flow tagging to a high Reynolds number, Mach 3 blow-down air facility at Princeton University's Gas Dynamics Laboratory. RELIEF tagging was accomplished using stimulated Raman scattering to vibrationally excited oxygen molecules. Examples include instantaneous images of boundary-layer structure and shock-wave/boundary-layer interactions, as well as results of flow tagging velocity measurements in the free-stream and boundary-layer regions of this facility. The future implementation of filtered Rayleigh scattering is also discussed.

KW - filtered Rayleigh scattering

KW - RELIEF flow tagging

KW - Mach 3 blow-down air facility

KW - stimulated Raman scattering

KW - flow tagging

UR - http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=883

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DO - 10.1109/ICIASF.1991.186247

M3 - Conference contribution book

SP - 255

EP - 261

BT - International Congress on Instrumentation in Aerospace Simulation Facilities, 1991

PB - IEEE

CY - Piscataway, NJ, United States

ER -

Rayleigh imaging and flow tagging in ground test facilities

Abstract

Keywords

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