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Experimental and analytical investigation of fast normal shock position controls for a Mach 2.5 mixed-compression inlet

机译：马赫2.5混合压缩入口快速正常冲击位置控制的实验和分析研究

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Normal shock control systems for supersonic mixed compression inlet using feedback loops

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作者
Cole, G. L.; Crosby, M. J.; Neiner, G. H.;
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年度 1971
页码 1-64
总页数 64
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIR INTAKES; FEEDBACK CONTROL; NORMAL SHOCK WAVES; INTAKE SYSTEMS; PRESSURE RECOVERY; SUPERSONIC WIND TUNNELS; TURBOJET ENGINES;

机译：空气进入;反馈控制;正常冲击波;进口系统;压力恢复;超级风洞;涡轮发动机;

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专利

1. Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward Highlight and Bleed Slot in an Inverted 'X'-type Layout [J] . Wan Dawei, Guo Rongwei Chinese journal of aeronautics . 2007,第4期

机译：固定几何二维混合压缩超音速进气口，前掠高光和排气槽呈倒“ X”型布局
2. Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward High-light and Bleed Slot in an Inverted "X"-type Layout [J] . Wan Dawei, Guo Rongwei 中国航空学报（英文版） . 2007,第004期

机译：固定几何二维混合压缩超音速进气口，其前掠高光和排气槽呈倒“ X”型布局
3. Experimental Investigation of the Weak Shock Wave Influence on the Boundary Layer of a Flat Blunt Plate at the Mach Number 2.5 [J] . Ermolaev Yu. G., Kosinov A. D., Kocharin V. L., Fluid Dynamics . 2019,第2期

机译：MACH编号2.5扁平钝板边界层弱冲击波影响的实验研究
4. Experimental Investigation on Mixed-Compression Inlet of Solid Fuel Ramjet Projectile [C] . Bo SUN, Xiaosong WU, Qiang XIA, The Third International Conference on Mechanical Engineering and Mechanics(第三届国际机械工程与力学会议）论文集 . 2009

机译：固体燃料冲压喷气弹混合压缩入口的实验研究
5. Hypersonic mixed-compression inlet shock-induced combustion ramjets. [D] . Alexander, Derrick. 2006

机译：高超声速混合压缩进气口冲击诱发的燃烧冲压发动机。
6. Flow visualisation of a normal shock impinging over a rounded contour bump in a Mach 1.3 free-stream [O] . Kin Hing Lo, Konstantinos Kontis -1

机译：撞击在Mach 1.3自由流中的圆形轮廓凸起上的正常冲击的流动可视化
7. Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10: A Computational and Experimental Investigation [O] . Holland Scott D. 1992

机译：通用侧壁压缩超燃冲压发动机进气口在10马赫时的雷诺数和风帽位置影响：计算和实验研究
8. Experimental and Analytical Investigation of Fast Normal Shock Position Controls for a Mach 2.5 Mixed-Compression Inlet [R] . Cole, G. L., Crosby, M. J., Neiner, G. H. 1971

机译：马赫2.5混合压缩入口快速正常冲击位置控制的实验与分析研究

Experimental and analytical investigation of fast normal shock position controls for a Mach 2.5 mixed-compression inlet

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