The effects of vane-type tabs on flow and acoustic fields of supersonic jet
Author:
Affiliation:
1. Nagoya Univ., Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-87
Reference9 articles.
1. K. K. AhujaandW. H. Brown,"Shear.flow controlby mechanicaltabs,0022,AIAA Paper89-0994,1989.
2. Spreading characteristics of compressible jets from nozzles of various geometries
3. Effect of tabs on the flow and noise field of an axisymmetric jet
4. Control of an axisymmetric jet using vortex generators
5. On the Mechanism of Choked Jet Noise
Cited by 3 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. Jet noise reduction using co-axial swirl flow with curved vanes;Applied Acoustics;2017-11
2. Noise Reduction in a Non-Ideally Expanded Round Jet via Steady Blowing;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
3. Effects of Nozzle Trailing Edges on Acoustic Field of Supersonic Rectangular Jet;AIAA Journal;2001-06
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