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Research on supersonic combustion

Published:1993-07 Issue:4 Volume:9 Page:499-514
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Billig F. S.¹

Affiliation:

1. Johns Hopkins University, Laurel, Maryland 20723

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.23652

Reference162 articles.

1. Kinetics Wall cooling 62-68 69-83 24-90 19b, 24e, 29, 31, 41, 91-103 9, 104-112 9, 113-115 26, 27, 52, 115-121 122-125 Modeling of flow structure3Coupling of integral and finite

2. Free-jet engine tests317b, 52, 54, 58, 63, 130-134

3. 135-137 16, 17c, 18b,35, 51

4. 138-145

5. 58, 60, 61, 146-150

Cited by 357 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. Thermodynamic analysis on the performance of hydrocarbon fueled scramjet with inlet active cooling;Energy;2024-11

2. Wavelet optical flow velocimetry of a scramjet combustor using high-speed frame-straddling focusing schlieren images;Combustion and Flame;2024-11

3. Combustion performance of hydrogen fueled parallel wall-jet used for drag reduction in a supersonic combustor;Case Studies in Thermal Engineering;2024-07

4. Experimental investigation of mode transition process in a cavity-based scramjet;Physics of Fluids;2024-04-01

5. Shock-induced supersonic combustion with a streamwise vortex;Physics of Fluids;2024-03-01

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