A comparative study of scramjet injection strategies for high Mach numbers flows

Author:

RIGGINS D.1,MCCLINTON C.2,ROGERS R.2,BITTNER R.3

Affiliation:

1. Missouri-Rolla, University, Rolla

2. NASA, Langley Research Center, Hampton, VA

3. Analytical Services and Materials, Inc., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

Cited by 8 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. Effect of Geometrical Parameters on the Mixing Performance of Cantilevered Ramp Injectors;AIAA Journal;2003-03

2. Evaluation of hypersonic fuel/air mixing performance by cantilevered ramp injectors;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

3. On the bridge from hypersonic aeropropulsion ground test data to flight performance;20th AIAA Advanced Measurement and Ground Testing Technology Conference;1998-06-15

4. Advanced turbulence models for high-Mach number wall bounded flows;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

5. Computational modeling of mixing process for scramjet combustor applications;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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