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Large scale supersonic combustor testing at conditions simulating Mach 8 flight

机译：在模拟8马赫飞行条件下的大型超声波燃烧器测试

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Large scale supersonic combustor testing at conditions simulating Mach 8 flight

机译：在模拟8马赫飞行条件下的大型超声波燃烧器测试

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Mertz T. W.; Metzler A. J.;
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年度 1970
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1. Ignition and combustion characteristics of supersonic combustor under flight Mach number 2.6-3.8 [J] . Li Jianping, Wang Kai, Jiao Guiqian, Fuel . 2021,第Jana1期

机译：在飞行马赫编号2.6-3.8下的超音速燃烧器的点火和燃烧特性
2. Design of a Mach 2 shape transition nozzle for lab-scale direct-connect supersonic combustor [J] . Sung Bu-Kyeng, Choi Jeong-Yeol Aerospace science and technology . 2021,第Octa期

机译：用于实验室直接连接超声波燃烧器的Mach 2形过渡喷嘴的设计
3. 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
4. Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight [C] . M. Takahashi, T. Komuro, K. Sato, AIAA International Space Planes and Hypersonic Systems and Technologies Conference . 2008

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
5. Development and ground testing of direct measuring skin friction gages for high enthalpy supersonic flight tests. [D] . Smith, Theodore Brooke. 2001

机译：直接测量皮肤摩擦计的开发和地面测试，用于高焓超音速飞行测试。
6. Measurement invariance tests of revisions to archaically worded items in the Mach IV scale [O] . Brian K. Miller, Kay Nicols, Robert Konopaske, 2012

机译：对Mach IV量表中的古文字项目进行修订的测量不变性测试
7. A hot gas generator for large scale supersonic combustor testing [O] . Metzler A. J., Lezberg E. A. 1968

机译：用于大型超声波燃烧器测试的热气发生器
8. Large Scale Supersonic Combustor Testing at Conditions Simulating Mach 8 Flight [R] . Mertz, T. W., Metzler, A. J. 1970

机译：模拟8马赫飞行条件下的大型超音速燃烧室试验

Large scale supersonic combustor testing at conditions simulating Mach 8 flight

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