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Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle

机译：在飞行试验车上安装的超音速涡轮喷气发线发动机的射击试验

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《American Institute of Aeronautics and Astronautics/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference》|2009年||共11页
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H. Taguchi; K. Harada; H. Kobayashi; T. Kojima; M. Hongoh; D. Masaki; S. Sawai; Y. Maru; T. Sato;
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中图分类各类型航空器;
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专利

1. Turbojet Runs Are Precursor to Hypersonic Engine Heat Exchanger Tests [J] . Guy Norris Aviation Week & Space Technology . 2018,第10期

机译：涡轮喷气发动机运行是超音速发动机热交换器测试的先驱
2. DESIGN STUDY AND COMPONENT TESTS ON A SUBSCALE PRECOOLED TURBOJET ENGINE FOR FLIGHT EXPERIMENTS [J] . Hideyuki Taguchi, Takayuki Kojima, Kazuhisa Fijita, Space technology . 2006,第1a2期

机译：用于飞行实验的超小型预冷却涡轮喷气发动机的设计研究和组件测试
3. Development study of precooled-cycle hypersonic turbojet engine for flight demonstration [J] . Tetsuya Sato, Hideyuki Taguchi, Hiroaki Kobayashi, Acta astronautica . 2007,第1a6期

机译：用于飞行演示的预冷循环高超音速涡轮喷气发动机的开发研究
4. Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle [C] . H. Taguchi, K. Harada, H. Kobayashi, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference . 2009

机译：安装在飞行测试飞行器上的超音速涡轮喷气发动机的点火测试
5. A DETAILED PROCEDURE FOR MEASURING TURBOJET ENGINE PERFORMANCE IN AN ENCLOSED SEA-LEVEL TEST FACILITY. [D] . RUDNITSKI, DONALD MICHAEL 1983

机译：在封闭海级测试设施中测量涡轮喷气发动机性能的详细过程。
6. Indoor and Outdoor Tests for a Chemi-capacitance CarbonNanotube Sensor Installed on a Quadrotor Unmanned Aerial Vehicle forDimethyl Methylphosphonate Detection and Mapping [O] . Jong-Seon Kim, *, ‡, 2021

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7. Effects of forward velocity on noise for a J85 turbojet engine with multitube suppressor from wind tunnel and flight tests [O] . Stone, J. R., Miles, J. H., Sargent, N. B. 1976

机译：风洞和飞行试验中前向速度对带有多管抑制器的J85涡轮喷气发动机噪声的影响
8. Ground Test and Computation of Boundary Layer Transition on the Hypersonic International Flight Research and Experimentation (HIFiRE)-5 Vehicle. [R] . Kimmel, R., Adamczak, D., Gosse, R., 2011

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