Flow characteristics of a trapped-vortex pilot cavity under the influence of radial structure-Reference-Cited by-同舟云学术

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Flow characteristics of a trapped-vortex pilot cavity under the influence of radial structure

Published:2023-10 Issue: Volume:148 Page:110974
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Zhang Yuxuan,He Xiaomin^ORCID

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference26 articles.

1. Performance of a trapped-vortex combustor;Hsu,1995

2. Experimental study of compact ram combustor with double-staged flameholders for ATR engine;Hasegawa,2001

3. Lee J, Winslow R, Buehrle B J. The GE- NASA RTA Hyperburner Design and Development. Washington,D.C.:NASA;2005. Report No.: NASA/TM-2005-213803.

4. Revolutionary turbine accelerator (RTA) demonstrator;McNelis,2005

5. Cottle AE, Gilbert NA, Polanka MD. Mechanisms for enhanced flow migration from an annular, high-g ultra compact combustor. Reston:AIAA;2016. Report No.: AIAA-2016-1392.

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1. Spray and flame characteristics of an ultra-compact combustor for gas turbines;Applied Thermal Engineering;2024-12

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