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Visualization of Wake Flows over High-Angles-of-Attack Delta Configurations at Supersonic and Hypersonic Speeds

机译：在超音速和超声波速度下，可视化唤醒在高角度的攻击Δ配置上流动

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Kojiro SUZUKI; Daisuke HAGISHIMA; Kazuhiko YAMADA; Motoyuki HONGOH;
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年度 2002
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1. Nonintrusive measurements for high-speed, supersonic, and hypersonic flows [Review] [J] . Bonnet JP., Taran JP., Gresillon D. Annual Review of Fluid Mechanics . 1998,第0期

机译：高速，超音速和高音速流的非侵入式测量[综述]
2. Three-dimensional effects on line-of-sight visualization measurements of supersonic and hypersonic flow over cylinders [J] . Troy N. Eichmann, Timothy J. McIntyre, Alexis I. Bishop, Shock Waves . 2007,第4a5期

机译：汽缸上超音速和高音速流的视线可视化测量中的三维效应
3. Three-dimensional effects on line-of-sight visualization measurements of supersonic and hypersonic flow over cylinders [J] . Eichmann TN, McIntyre TJ, Bishop AI, Shock Waves . 2007,第4a5期

机译：汽缸上超音速和高音速流的视线可视化测量中的三维效应
4. Calculation method for supersonic/hypersonic flows over configurations with blunt leading edges [C] . Dr.N.V.Voevodenko 1st AIAA Aircraft Engineering, Technology, and Operations Congress September 19-21, 1995/Los Angeles, CA . 1995

机译：超音速/超音速流动的计算方法，前缘钝化
5. FLOW FIELD AND STABILITY OF THE FAR WAKE BEHIND CYLINDERS AT HYPERSONIC SPEEDS. [D] . BEHRENS, HERMANN WILHELM. 1966

机译：超音速汽缸后远尾流场的流场和稳定性。
6. Visualization of Intraaneurysmal Flow Patterns with Transluminal Flow Images of 3D MR Angiograms in Conjunction with Aneurysmal Configurations [O] . Toru Satoh, Keisuke Onoda, Shoji Tsuchimoto 2003

机译：具有三维MR血管造影的透气性图像与动脉瘤配置的透气流模型的可视化
7. Laminar boundary layer separation and near wake flow for a smooth blunt body at supersonic and hypersonic speeds [O] . Grange Jean-Marie 1966

机译：层流边界层分离和近尾流在超音速和高超音速下为平滑钝体提供
8. Research on Hypersonic Flow of Blunt delta Wings. Part III. Gap Effects of a Blunt Slab delta Wing at Moderate Supersonic and Hypersonic Speeds [R] . Mazelsky, B., Chao, C. C. 1968

机译：钝三角翼高超声速流动研究。第三部分。平板超音速和高超音速速度下钝板三角翼的间隙效应

Visualization of Wake Flows over High-Angles-of-Attack Delta Configurations at Supersonic and Hypersonic Speeds

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