Numerical simulation of gas turbine swirl-stabilized injector dynamics

Author:

Wang Shanwu1,Hsieh Shih-Yang1,Yang Vigor1

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Toward the large-eddy simulation of compressible turbulent flows

2. A-A t=21.01ms 1321 2031 3123 4802 7384 t=21.04ms Fig.2Grid system

Cited by 4 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. Fuel effects on the performance of a recirculation-zone supported burner;54th AIAA Aerospace Sciences Meeting;2016-01-02

2. C/H atom ratio in recirculation-zone-supported premixed and nonpremixed flames;Proceedings of the Combustion Institute;2013

3. Unsteady Flow Structures in Radial Swirler Fed Fuel Injectors;Journal of Engineering for Gas Turbines and Power;2004-03-01

4. Vortical dynamics and acoustic response in gas-turbine swirl-stabilized injectors;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

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