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Transition Measurement Using Hot-Film on Supersonic Experimental Airplane NEXST-1

机译：超音速实验飞机NEXsT-1上使用热膜的过渡测量

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作者
Togkugawa, N.; Yoshida, K.;
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年度 2007
页码 p.1-71
总页数 71
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aircraft; Flight tests; Validation; Laminar flow; Sensors;

机译：飞机;飞行试验;验证;层流;传感器;

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专利

1. TRANSITION MEASUREMENT OF NATURAL LAMINAR FLOW WING ON SUPERSONIC EXPERIMENTAL AIRPLANE NEXST-1 [J] . Naoko Tokugawa Noise & vibration bulletin . 2009,第2期

机译：超音速实验飞机NEXST-1上自然层流翼的过渡测量
2. Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1 [J] . Naoko Tokugawa, Dong-Youn Kwak, Kenji Yoshida, Journal of Aircraft . 2008,第5期

机译：超音速实验飞机NEXST-1上自然层流翼的过渡测量
3. Numerical Analysis on Flight-Test Results of Supersonic Experimental Airplane NEXST-1 [J] . Hiroaki Ishikawa, Dong-Youn Kwak, Kenji Yoshida Journal of Aircraft . 2008,第5期

机译：超音速实验飞机NEXST-1飞行测试结果的数值分析
4. TRANSITION MEASUREMENT SYSTEM OF EXPERIMENTAL SUPERSONIC TRANSPORT 'NEXST-1' [C] . Naoko Tokugawa, Dong-Youn Kwak, Kenji Yoshida Congress of the International Council of the Aeronautical Sciences . 2006

机译：实验超音速运输的过渡测量系统'NEXST-1'
5. Experimental probes of gas phase ions and molecules: I. Product kinetic energy release measurements as a probe of reaction thermochemistry, dynamics, and chemical structure in systems containing transition metal ions. II. Photoelectron and optical studies of organic transient species. [D] . Dearden, David Vernell. 1989

机译：气相离子和分子的实验探针：I.产物动能释放测量，作为包含过渡金属离子的系统中反应热化学，动力学和化学结构的探针。二。有机瞬态物质的光电子和光学研究。
6. A Flexible Hot-Film Sensor Array for Underwater Shear Stress and Transition Measurement [O] . Baoyun Sun, Pengbin Wang, Jian Luo, 2018

机译：用于水下剪切应力和过渡测量的柔性热膜传感器阵列
7. A Flexible Hot-Film Sensor Array for Underwater Shear Stress and Transition Measurement [O] . Baoyun Sun, Pengbin Wang, Jian Luo, 2018

机译：用于水下剪切应力和过渡测量的柔性热胶片传感器阵列
8. Demonstration of Aerodynamic Design Technologies on Supersonic Experimental Airplane (NEXST-1) by Flight Test [R] . Kwak, D. Y., Tokugawa, N., Yoshida, K., 2007

机译：用飞行试验证明超音速实验飞机（NEXsT-1）的空气动力学设计技术

Transition Measurement Using Hot-Film on Supersonic Experimental Airplane NEXST-1

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