The investigation of operation domain of strut fuel feed system for model scramjet combustor

机译：超燃冲压发动机燃烧器支撑燃料供给系统的工作范围研究

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From the results of experimental studies of model combustors in wind tunnels with connected pipe and as a part of autonomous module, the relationships are revealed and the criteria for probability estimation of ignition and stable combustion of hydrogen and hydrocarbon fuel in scramjet combustor with pylon fuel injection system are developed.

机译：从连接管的风洞中模型燃烧器的实验研究结果作为自主模块的一部分，揭示了两者之间的关系，并确定了喷射喷射燃料燃烧器中采用塔式燃料喷射的氢和碳氢燃料的着火和稳定燃烧的概率估计标准。系统开发。

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《AIAA international space planes and hypersonic systems and technologies conference》|1998年|p.83-92|共10页
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V.Semenov; O.Romankov;
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中图分类各类型航空器;
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4. The investigation of operation domain of strut fuel feed system for model scramjet combustor [C] . Semenov, V. L. In: AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 8th, Norfolk, VA, Apr. 27-30, 1998, Collection of Technical Papers (A98-27876 06-15), Reston, VA, American Institute of Aeronautics and Astronautics, 1998 . 1998

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The investigation of operation domain of strut fuel feed system for model scramjet combustor

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