Vorticity generation mechanisms in parallel injection schemes for supersonic mixing-Reference-Cited by-同舟云学术

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Vorticity generation mechanisms in parallel injection schemes for supersonic mixing

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

DONOHUE JAMES¹,HAJ-HARIRI HOSSEIN¹,MCDANIEL, JR. JAMES¹

Affiliation:

1. Virginia, University, Charlottesville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3286

Reference12 articles.

Cited by 11 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. Investigation of strut-ramp injector in a Scramjet combustor: Effect of strut geometry, fuel and jet diameter on mixing characteristics;Journal of Mechanical Science and Technology;2017-03

2. Effect of Trailing Ramp Angles in Strut-Based Injection in Supersonic Flow;Journal of Propulsion and Power;2013-01

3. Strut-Based Gaseous Injection into a Supersonic Stream;Journal of Propulsion and Power;2006-03

4. Mixing and combustion in scramjet combustor with raised and relieved ramp;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

5. Effects of ramp swept angle in supersonic mixing;21st Aerodynamic Measurement Technology and Ground Testing Conference;2000-06-19

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