Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight

机译：10马赫飞行超高速条件下超燃冲压发动机燃烧器性能的改进

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《AIAA International Space Planes and Hypersonic Systems and Technologies Conference》|2008年|P.1-6|共6页
会议地点 Dayton OH(US)
作者
M. Takahashi; T. Komuro; K. Sato; M. Kodera; H. Tanno; K. Itoh;
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Japan Aerospace Exploration Agency Tsukuba Japan;

Japan Aerospace Exploration Agency Kakuda Japan;

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1. Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition [J] . Sun M.B., Gong C., Zhang S.P., Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics . 2012,第Null期

机译：在氢气驱动下并配备多腔的超燃冲压燃烧器中的火花点火过程，飞行速度为4马赫
2. Suppression of Combustor-Inlet Interaction in a Scramjet Engine under Mach 4 Flight Conditions [J] . Kan Kobayashi, Takeshi Kanda, Sadatake Tomioka, Transactions of the Japan society for aeronautical and space sciences . 2007,第166期

机译：在4马赫飞行条件下超燃冲压发动机中燃烧器-进气道相互作用的抑制
3. Effect of the reaction mechanism on the numerical prediction of the performance of a scramjet combustor at cruise flight 8 Mach number [J] . Santana Edder Rabadan, Weigand Bernhard Aerospace science and technology . 2021,第May期

机译：反应机制对巡航飞行8马赫数跳闸燃烧器性能数值预测的影响
4. Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight [C] . AIAA International Space Planes and Hypersonic Systems and Technologies Conference . 2008

机译：超速条件下的Scramjet燃烧器性能的改进
5. Experimental investigation of an ejector scramjet RBCC at Mach 4.0 and 6.5 simulated flight conditions. [D] . Nelson, Karl William. 2002

机译：在4.0和6.5马赫模拟飞行条件下对超燃冲压发动机RBCC进行的实验研究。
6. Investigations on the Influence of the In-Stream Pylon and Strut on the Performance of a Scramjet Combustor [O] . Hao Ouyang, Weidong Liu, Mingbo Sun -1

机译：流内塔架和支柱对超燃冲压燃烧器性能的影响研究
7. An experimental investigation of an airframe integrated three-dimensional scramjet engine at a Mach 10 flight condition [O] . Doherty Luke James 2014

机译：在10马赫飞行条件下机体集成三维超燃冲压发动机的实验研究
8. Thermal Performance of a Scramjet Combustor Operating at Mach 5.6 Flight Conditions [R] . Stouffer, S. D. , Neumann, R. D. , Emmer, D. S. 1997

机译：以5.6马赫飞行条件运行的超燃冲压发动机燃烧室的热性能

Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight

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