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Wind Tunnel Testing of an Axisymmetric Isentropic Relaxed External Compression Inlet at Mach 1.97 Design Speed

机译：设计速度为1.97马赫的轴对称各向同性松弛外部压缩入口的风洞测试

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《AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit》|2007年|P.1-12|共12页
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作者
T. Conners; J. Merret; D. Howe; K. Tacina; S. Hirt;
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中图分类航空发动机（推进系统）;
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1. Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression [J] . Galkin V. M., Vnuchkov D. A., Zvegintsev V. I. Journal of Applied Mechanics and Technical Physics . 2015,第5期

机译：等轴压缩轴对称隧道进气口的气动设计
2. On the question of starting conditions for frontal axisymmetric inlets tested in hot-shot wind tunnels [J] . Yu.P. Gounko, I.I. Mazhul Thermophysics and Aeromechanics . 2017,第3期

机译：在热射流隧道中进行正面轴对称入口的启动条件问题
3. Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression [J] . Chen Hao, Tan Hui-Jun, Zhang Qi-Fan, AIAA Journal . 2017,第12期

机译：部分等熵压缩的外部压缩入口中的嗡嗡声流
4. Wind Tunnel Testing of an Axisymmetric Isentropic Relaxed External Compression Inlet at Mach 1.97 Design Speed [C] . T. Conners, J. Merret, D. Howe, AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2007

机译：Mach 1.97设计速度的轴对称等熵宽松外压缩入口的风洞测试
5. External aerodynamics of heavy ground vehicles: Computations and wind tunnel testing. [D] . Bayraktar, Ilhan. 2002

机译：重型地面车辆的外部空气动力学：计算和风洞测试。
6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

机译：利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
7. CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet [O] . Conners Timothy R., Tacina Kathleen M., Hirt Stefanie M., 2008

机译：轴对称各向同性松弛压缩入口的CFD结果
8. PERFORMANCE OF A MACH NUMBER 3.0 DESIGN AXISYMMETRIC DOUBLE-CONE EXTERNAL-COMPRESSION INLET IN THE MACH NUMBER RANGE 1.97 TO 0.79 [R] . Davis, O. H., Mitchell, G. A. 1960

机译：maCH号3.0设计轴对称双锥体外压缩进口在机械编号范围1.97至0.79的性能

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