Experimental study of velocity flow field for a multiple swirl spray combustor-Reference-Cited by-同舟云学术

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Experimental study of velocity flow field for a multiple swirl spray combustor

Published:2002-01-14 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA Aerospace Sciences Meeting & Exhibit
language:
Short-container-title:

Author:

Li G.¹,Angier S.,Lambolez O.,Gutmark E.,Drouin B.

Affiliation:

1. Cincinnati, Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-618

Reference25 articles.

1. Wisler, D., Mongia, H. C, Held, T.,2001, "Control of Multiswirler Combustor", Private Communication.

2. Combustion instability related to vortex shedding in dump combustors and their passive control

3. Excitation of Thermoacoustic Instabilities by Interaction of Acoustics and Unstable Swirling Flow

4. The Theory of Sound

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Combustor technology of high temperature rise for aero engine;Progress in Aerospace Sciences;2023-07

2. Effect of dilution holes on the performance of a triple swirler combustor;Chinese Journal of Aeronautics;2014-12

3. A Comparative Study of Flamelet and Finite Rate Chemistry LES for a Swirl Stabilized Flame;Journal of Engineering for Gas Turbines and Power;2012-01-27

4. Experimental Study on Coherent Structures of a Counter-rotating Multi-Swirler Cup;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

5. Recent Advances in the Development of Combustor Design Tools;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

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