Supersonic combustion experiments for CFD model development and validation (invited)

A. D. Cutler; P. M. Danehy; S. O'Byrne; C. G. Rodriguez; J. P. Drummond

doi:10.2514/6.2004-266

Supersonic combustion experiments for CFD model development and validation (invited)

A. D. Cutler^*, P. M. Danehy, S. O'Byrne, C. G. Rodriguez, J. P. Drummond

^*Corresponding author for this work

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

10 Citations (Scopus)

Abstract

This paper briefly reviews a number of experiments suitable for the screening, development and validation of turbulence models used in computational fluid dynamics (CFD). Then, two sets of experiments conducted for this purpose by the authors are presented. The first is a compressible axisymmetric jet in which a central jet of helium mixes with a surrounding coflow of air. The second is a supersonic combustor. Various instrumentation techniques have been employed with the axisymmetric jet, whereas the dual pump coherent anti-Stokes Raman spectroscopy technique has been applied to the combustor. Experiences in trying to calculate these flows, and set model constants, are reviewed.

Original language	English
Pages	2704-2716
Number of pages	13
DOIs	https://doi.org/10.2514/6.2004-266
Publication status	Published - 2004
Externally published	Yes
Event	42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: 5 Jan 2004 → 8 Jan 2004

Conference

Conference	42nd AIAA Aerospace Sciences Meeting and Exhibit
Country/Territory	United States
City	Reno, NV
Period	5/01/04 → 8/01/04

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10.2514/6.2004-266

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title = "Supersonic combustion experiments for CFD model development and validation (invited)",

abstract = "This paper briefly reviews a number of experiments suitable for the screening, development and validation of turbulence models used in computational fluid dynamics (CFD). Then, two sets of experiments conducted for this purpose by the authors are presented. The first is a compressible axisymmetric jet in which a central jet of helium mixes with a surrounding coflow of air. The second is a supersonic combustor. Various instrumentation techniques have been employed with the axisymmetric jet, whereas the dual pump coherent anti-Stokes Raman spectroscopy technique has been applied to the combustor. Experiences in trying to calculate these flows, and set model constants, are reviewed.",

author = "Cutler, {A. D.} and Danehy, {P. M.} and S. O'Byrne and Rodriguez, {C. G.} and Drummond, {J. P.}",

year = "2004",

doi = "10.2514/6.2004-266",

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note = "42nd AIAA Aerospace Sciences Meeting and Exhibit ; Conference date: 05-01-2004 Through 08-01-2004",

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AU - Cutler, A. D.

AU - Danehy, P. M.

AU - O'Byrne, S.

AU - Rodriguez, C. G.

AU - Drummond, J. P.

PY - 2004

Y1 - 2004

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AB - This paper briefly reviews a number of experiments suitable for the screening, development and validation of turbulence models used in computational fluid dynamics (CFD). Then, two sets of experiments conducted for this purpose by the authors are presented. The first is a compressible axisymmetric jet in which a central jet of helium mixes with a surrounding coflow of air. The second is a supersonic combustor. Various instrumentation techniques have been employed with the axisymmetric jet, whereas the dual pump coherent anti-Stokes Raman spectroscopy technique has been applied to the combustor. Experiences in trying to calculate these flows, and set model constants, are reviewed.

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DO - 10.2514/6.2004-266

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T2 - 42nd AIAA Aerospace Sciences Meeting and Exhibit

Y2 - 5 January 2004 through 8 January 2004

ER -

Supersonic combustion experiments for CFD model development and validation (invited)

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