An Electromagnetic Shock Tube for Aerodynamic Research

机译：一种用于空气动力学研究的电磁激波管

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摘要

An electromagnetically driven shock tube was studied as a possible new tool for aerodynamic research in which velocities of up to 41,000 feet per second are obtainable in air. At these high velocities stagnation temperatures of about 35,000K are produced. The simple construction and operation of the shock tube is described and an evaluation is made of its performance. The potentialities and limitations of the apparatus are discussed with regards to research applications. The results of some magnetoaerodynamic studies are presented to show the usefulness of this type of shock tube. (Author)

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Ziemer, R. W.;
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年度 1958
页码 p.1-2
总页数 2
原文格式 PDF
正文语种 eng
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关键词
SHOCK TUBES ; ELECTROMAGNETISM ; AERODYNAMIC CHARACTERISTICS ; SCIENTIFIC RESEARCH ; OPERATION ; ELECTRIC DISCHARGES ; MAGNETIC PINCH ; MAGNETOHYDRODYNAMICS ; PERFORMANCE (ENGINEERING) ; DESIGN;

机译：冲击管;电磁学;空气动力学特性;科学研究;操作;电子放电;磁性夹;磁流体动力学;性能（工程）;设计;

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2. Experiment on low-frequency electromagnetic waves propagating in shock-tube-generated magnetized cylindrical enveloping plasma [J] . Shaoshuai GUO, Kai XIE, Bin SUN, 等离子体科学和技术（英文版） . 2021,第007期
3. Modeling and experimental study of low-frequency electromagnetic wave propagation in cylindrical enveloping plasma produced by a shock tube [J] . Xie Kai, Guo Shaoshuai, Sun Bin, Physics of plasmas . 2019,第7期

机译：冲击管产生圆柱包络等离子圆柱包装等离子体中低频电磁波传播的建模与实验研究
4. Experimental Investigations of an Aerodynamic Flow of Geometrical Models in Hypersonic Aerodynamic Shock Tube [C] . M.A. Kotov, I.A. Kryukov, L.B. Ruleva, AIAA applied aerodynamics conference . 2013

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5. In Situ Probe-Enabled Tunable Diode Laser Absorption Measurements in Flames, Shock Tubes and Shock Tunnels [D] . Girard, Julian Jon Laurent. 2021

机译：在火焰，冲击管和冲击隧道中启用了启用探针的可调谐二极管激光吸收测量
6. THE SHOCK TUBE IN AERODYNAMIC AND STRUCTURAL RESEARCH [O] . H. G. Stever, R. L. Bisplinghoff 1954

机译：气动和结构研究中的冲击管
7. Investigations of the Aerodynamic Characteristics of the Shock Tubes : Part 4, Aerodynamic Characteristics of Laval Nozzles Installed in a Shock Tube [O] . Takefumi IKUl, Kazuyasu MATSUO 1972

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8. Plasma Flow in an Electromagnetic Shock Tube and in a Compression Shock Tube [R] . J. L Wilson, D. Schofield, J. D. Regan 1966

机译：电磁冲击管和压缩激波管中的等离子体流动

An Electromagnetic Shock Tube for Aerodynamic Research

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