Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure-Reference-Cited by-同舟云学术

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Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Mariani Raffaello¹,Kontis Konstantinos¹

Affiliation:

1. University of Manchester

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-410

Reference21 articles.

1. Spreading characteristics of compressible jets from nozzles of various geometries

2. 2Sheldon,I.G.,FluidVortices,KluwerAcademicPublisher,1995,Ch.7.

3. A universal time scale for vortex ring formation

4. The motion of a shock wave in a channel, with applications to cylindrical and spherical shock waves

Cited by 5 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. Influence of nozzle exit geometrical parameters on supersonic jet decay;International Journal of Turbo & Jet-Engines;2021-01-20

2. Influence of nozzle exit geometrical parameters on supersonic jet decay;International Journal of Turbo & Jet-Engines;2021-01-20

3. Vortex–shock and vortex–vortex interactions in the compressible starting jet from two beveled nozzle configurations;Journal of Visualization;2020-09-22

4. Shock-free compressible vortex rings impinging on a stationary surface: Effects of surface angle variation;Experimental Thermal and Fluid Science;2013-05

5. Experimental studies on coaxial vortex loops;Physics of Fluids;2010-12

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