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Influences of Angles of Attack and Sideslip on the Flow Field of a Cantilevered Ramp Injector in Supersonic Flows

机译：超声波流动悬臂坡道喷射器流动场上的攻击角度的影响

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Wei HUANG; Zhen-guo WANG; Wei-dong LIU; Shi-bin LI;
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年度 2014
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1. Influences of Angles of Attack and Sideslip on the Flow Field of a Cantilevered Ramp Injector in Supersonic Flows [J] . Wei Huang, Zhen-guo Wang, Wei-dong Liu, Transactions of the Japan society for aeronautical and space sciences . 2014,第4期

机译：攻角和侧滑对超声速流动中悬臂式斜坡喷射器流场的影响
2. Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows [J] . Wei Huang, Shi-bin Li, Li Yan, Acta astronautica . 2013,第MARaaAPRa期

机译：超声速悬臂式斜面喷油器性能评估与参数分析
3. A STUDY ON EFFECTS OF SHOCK IMPINGEMENT ON SUPERSONIC MIXING FLOW FIELD GENERATED BY PARALLEL INJECTION METHOD WITH A RAMP INJECTOR [J] . YOSHIYUKI YAMANE, SHIGERU ASO, SEIICHI SAWAGUCHI 日本航空宇宙学会論文集 . 1999,第544期

机译：冲击波对带有斜坡喷射器的平行注射法产生的超声速混合流场的影响研究
4. Complete 3-D multi-parameter mapping of the supersonic mixing flowfield of a ramp fuel injector [C] . J.M.Donohue, J.C.McDaniel AIAA 33rd Aerospace Seicnces Meeting and Exhibit January 9-12, 1995/Reno, NV . -1

机译：坡道喷油器的超音速混合流场的完整3D多参数映射
5. Numerical simulation of cantilevered ramp injector flow fields for hypervelocity fuel/air mixing enhancement. [D] . Schumacher, Jurgen Christian. 2000

机译：悬臂式坡道喷油器流场的数值模拟，用于增强超高速燃料/空气混合。
6. Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows [O] . X. Gao, G. X. Xiang, W. J. Tang, -1

机译：超音速流中双扫/双斜坡楔引起的复流研究
7. CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 – Part 2 [O] . C.J. Bennett, N.J. Lawson, J.E. Gautrey, 2017

机译：BAE喷射射流3102上攻击角度和侧滑角叶片流动的CFD仿真 - 第2部分
8. Calculation of Three-Dimensional Supersonic Flow Fields about Aircraft Fuselages and Wings at General Angle of Attack, [R] . chu, chong-wei 1973

机译：一般迎角下飞机架和机翼三维超音速流场的计算，

Influences of Angles of Attack and Sideslip on the Flow Field of a Cantilevered Ramp Injector in Supersonic Flows

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