Experimental study of isothermal swirling flows in a dump combustor

Author:

Samimy M.1,Langenfeld C. A.1

Affiliation:

1. Ohio State University, Columbus, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 18 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. An Experimental Investigation of Swirl Flow in Axial Acoustic Fields;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

2. Liner dome shape effect on the annulus flow characteristics with and without swirl for a can-combustor model;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2007-05-01

3. Swirler Flow Field Characteristics in a Sudden Expansion Combustor Geometry;Journal of Propulsion and Power;2006-07

4. Swirler Flow Field Characteristics in a Sudden Expansion Combustor Geometry Using PIV;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

5. Effect of swirl cup on characteristics of fuel spray in gas turbine combustors;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

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