3D flame measurements at 5 kHz on a jet fueled aviation combustor

Lin Ma; Xuesong Li; Min Wook Kang; Warren G. Lamont; Krishnakumar Venkatesan; Shawn Wehe

doi:10.1115/GT2015-42823

3D flame measurements at 5 kHz on a jet fueled aviation combustor

Lin Ma, Xuesong Li, Min Wook Kang, Warren G. Lamont, Krishnakumar Venkatesan, Shawn Wehe

Mechanical Engineering

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

1 Scopus citations

Abstract

This paper describes the measurements of threedimensional (3D) flame measurements at 5 kHz from an optically accessible, atmospheric combustor burning Jet A. The measurements were performed by 3D tomography of flame chemiluminescence emissions. Such measurements resolve the instantaneous flame topography generated by the combustor in all three spatial directions and at a temporal resolution of 5 kHz (0.2 ms), essentially providing 4D information about the combustor. This paper reports the measurement technique, the experimental implementation, the results and their expected use for the continued development of future combustor concepts.

Original language	English (US)
Title of host publication	Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards
Publisher	American Society of Mechanical Engineers (ASME)
ISBN (Electronic)	9780791856758
DOIs	https://doi.org/10.1115/GT2015-42823
State	Published - 2015
Event	ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Canada Duration: Jun 15 2015 → Jun 19 2015

Publication series

Name	Proceedings of the ASME Turbo Expo
Volume	6

Other

Other	ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
Country	Canada
City	Montreal
Period	6/15/15 → 6/19/15

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10.1115/GT2015-42823

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Ma, L., Li, X., Kang, M. W., Lamont, W. G., Venkatesan, K., & Wehe, S. (2015). 3D flame measurements at 5 kHz on a jet fueled aviation combustor. In Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards (Proceedings of the ASME Turbo Expo; Vol. 6). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT2015-42823

3D flame measurements at 5 kHz on a jet fueled aviation combustor. / Ma, Lin; Li, Xuesong; Kang, Min Wook; Lamont, Warren G.; Venkatesan, Krishnakumar; Wehe, Shawn.

Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo; Vol. 6).

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

Ma, L, Li, X, Kang, MW, Lamont, WG, Venkatesan, K & Wehe, S 2015, 3D flame measurements at 5 kHz on a jet fueled aviation combustor. in Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards. Proceedings of the ASME Turbo Expo, vol. 6, American Society of Mechanical Engineers (ASME), ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015, Montreal, Canada, 6/15/15. https://doi.org/10.1115/GT2015-42823

Ma L, Li X, Kang MW, Lamont WG, Venkatesan K, Wehe S. 3D flame measurements at 5 kHz on a jet fueled aviation combustor. In Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards. American Society of Mechanical Engineers (ASME). 2015. (Proceedings of the ASME Turbo Expo). https://doi.org/10.1115/GT2015-42823

Ma, Lin ; Li, Xuesong ; Kang, Min Wook ; Lamont, Warren G. ; Venkatesan, Krishnakumar ; Wehe, Shawn. / 3D flame measurements at 5 kHz on a jet fueled aviation combustor. Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo).

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abstract = "This paper describes the measurements of threedimensional (3D) flame measurements at 5 kHz from an optically accessible, atmospheric combustor burning Jet A. The measurements were performed by 3D tomography of flame chemiluminescence emissions. Such measurements resolve the instantaneous flame topography generated by the combustor in all three spatial directions and at a temporal resolution of 5 kHz (0.2 ms), essentially providing 4D information about the combustor. This paper reports the measurement technique, the experimental implementation, the results and their expected use for the continued development of future combustor concepts.",

author = "Lin Ma and Xuesong Li and Kang, {Min Wook} and Lamont, {Warren G.} and Krishnakumar Venkatesan and Shawn Wehe",

note = "Publisher Copyright: Copyright {\textcopyright} 2015 by ASME. Copyright: Copyright 2016 Elsevier B.V., All rights reserved.; ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 ; Conference date: 15-06-2015 Through 19-06-2015",

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N2 - This paper describes the measurements of threedimensional (3D) flame measurements at 5 kHz from an optically accessible, atmospheric combustor burning Jet A. The measurements were performed by 3D tomography of flame chemiluminescence emissions. Such measurements resolve the instantaneous flame topography generated by the combustor in all three spatial directions and at a temporal resolution of 5 kHz (0.2 ms), essentially providing 4D information about the combustor. This paper reports the measurement technique, the experimental implementation, the results and their expected use for the continued development of future combustor concepts.

AB - This paper describes the measurements of threedimensional (3D) flame measurements at 5 kHz from an optically accessible, atmospheric combustor burning Jet A. The measurements were performed by 3D tomography of flame chemiluminescence emissions. Such measurements resolve the instantaneous flame topography generated by the combustor in all three spatial directions and at a temporal resolution of 5 kHz (0.2 ms), essentially providing 4D information about the combustor. This paper reports the measurement technique, the experimental implementation, the results and their expected use for the continued development of future combustor concepts.

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3D flame measurements at 5 kHz on a jet fueled aviation combustor

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