首页> 美国政府科技报告 >TOTAL-PRESSURE-RECOVERY CHARACTERISTICS OF A MODEL OF THE MCDONNELL XF3H-1 INLETS AND FOREBODY IN A FREE JET AT A MACH NUMBER OF 1.55

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TOTAL-PRESSURE-RECOVERY CHARACTERISTICS OF A MODEL OF THE MCDONNELL XF3H-1 INLETS AND FOREBODY IN A FREE JET AT A MACH NUMBER OF 1.55

机译：mCDONNELL XF3H-1入口和体内模型的总压力恢复特性在自由射流中的机器数为1.55

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作者
Carter, H. S.; Merlet, C. F.;
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年度 1952
页码 1-0
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原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ANGLE OF ATTACK; FOREBODIES; FREE JETS; HIGH SPEED; MACH NUMBER; YAW;

机译：攻击角度; FOREBODIEs;免费JETs;高速;马赫数;偏航;

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1. Investigation on gaseous jet in forebody/inlet for shock-induced combustion ramjet (shcramjet) engines [J] . Du Zhao-bo, Huang Wei, Yan Li Acta astronautica . 2018,第NOVa期

机译：冲击诱导燃烧冲压发动机（shcramjet）发动机前体/进气中的气体喷射研究
2. JET DROP MODELS FOR CONTROL OF NON-ISOTHERMAL FREE JETS IN A SIDE-WALL MULTI-INLET VENTILATION SYSTEM [J] . G. Zhang, J. S. Strøm Transactions of the ASAE . 1999,第4期

机译：侧墙多入口通风系统中非等温自由射流控制的射流滴模型
3. A hybrid CFD/characteristics method for fast characterization of hypersonic blunt forebody/inlet flow [J] . GAO WenZhi, LI ZhuFei, YANG JiMing 中国科学:物理学力学天文学（英文版） . 2015,第010期

机译：快速表征超声波钝头体/入口流动的混合CFD /特征方法
4. Investigation of Dynamic Characteristics for a Hypersonic Forebody/Inlet at Mach 6 [C] . Yu Anyuan, Le Jialing, Ni HongLi, Proceedings of 8th Sino-Russia high-speed flow conference . 2011

机译：马赫数为6的高超声速前体/进气口的动力特性研究
5. MACH REFLECTION, MACH DISC, AND THE ASSOCIATED NOZZLE FREE-JET FLOWS. [D] . CHANG, I-SHIH. 1973

机译：Mach反射，Mach光盘和相关的喷嘴自由流动。
6. Penetration Characteristics of Air Carbon Dioxide and Helium Transverse Sonic Jets in Mach 5 Cross Flow [O] . Erinc Erdem, Konstantinos Kontis, Selvaraj Saravanan 2014

机译：空气二氧化碳和氦气横向声速射流在5马赫错流中的渗透特性
7. Two-dimensional cascade tests of MCA blades in the high transonic Mach number region. 2nd report, On the effect of stagger angle on inlet Mach number characteristics. [O] . Hajime SAKAGUCHI, Susumu TAKAMORI 1990

机译：高跨音机马赫数区域的MCA叶片的二维级联试验。第2次报告，关于入口马赫数特征的错开角度。
8. Preliminary investigation of the total-pressure-recovery characteristics of a 15 degree semiangle movable-cone variable-geometry ram-jet inlet at free-jet Mach numbers of 1.62, 2.00, 2.53, and 3.05 [R] . Hinners, Arthur H , Jr, Lee, John B 1953

机译：自由喷射马赫数为1.62,2.00,2.53和3.05的15度半角可动锥可变几何冲压射流入口总压力恢复特性的初步研究

TOTAL-PRESSURE-RECOVERY CHARACTERISTICS OF A MODEL OF THE MCDONNELL XF3H-1 INLETS AND FOREBODY IN A FREE JET AT A MACH NUMBER OF 1.55

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