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Analytical investigation of supersonic turbomachinery blading. 2 - Analysis of impulse turbine-blade sections

机译：超音速涡轮机叶片的分析研究。 2 - 冲击式涡轮叶片部分的分析

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Surface Mach numbers, inlet flow angle, and specific heat ratio effects on geometric features of supersonic impulse turbine blade sections in Mach range 1.5 to 5.0

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作者
Goldman, L. J.;
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年度 1968
页码 1-23
总页数 23
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
SPACECRAFT POWER SUPPLIES; SUPERSONIC TURBINES; SYSTEMS ENGINEERING; TURBINE BLADES; FLOW GEOMETRY; INLET FLOW; SPECIFIC HEAT; SUPERSONIC FLOW; SURFACE GEOMETRY;

机译：航天电力供应;超音速涡轮;系统工程; TURBINE BLaDEs;流动几何;进水流量;特定热量;超音速流;表面几何;

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专利

1. Discussion on ????????Physical properties and impulse strength of paper????????, ????????The impulse strength of lapped impregnated paper dielectric???????? and ????????Breakdown under impulse voltages of solid and liquid dielectrics in combination???????? before the joint meeting of the Supply and Measurement and Control Sections, 25th April, 1956 [J] . Proceedings of the IEE - Part A: Power Engineering . 1956,第12期

机译：关于纸的物理性质和冲击强度的讨论搭接浸渍的纸介电材料的冲击强度结合固体和液体电介质的冲击电压击穿。在1956年4月25日供应与测量和控制部门联席会议之前
2. Turbulences of the supersonic gas flow during cold spraying and their negative effects: A DNS CFD analysis coupled with experimental observation and laser impulse high-speed shadowgraphs of the particles in-flight flow [J] . R. N. Raoelison, L. L Koithara, S. Costil, International Journal of Heat and Mass Transfer . 2020,第Feba期

机译：超音速气流在冷喷涂过程中的湍流及其负面影响：DNS CFD分析与实验观察以及飞行中粒子的激光脉冲高速阴影图相结合
3. Experimental and analytical investigation of the effects of single and multiple simulated lightning impulse currents on Metal-Oxide arrester blocks [J] . Jiang Anfeng, Fu Zhengcai, Sun Wei, Electric power systems research . 2016,第octa期

机译：单个和多个模拟雷电冲击电流对金属氧化物避雷器块影响的实验和分析研究
4. Supersonic COIL with iodine injection in transonic and supersonic sections of the nozzle [C] . S. Rosenwaks, E. Bruins, D. Furman, International symposium on gas flow and chemical lasers and high-power laser conference . 2001

机译：具有碘注射的超音速线圈，在喷嘴的横向和超音速部分
5. Aerodynamic inverse design of multistage turbomachinery blading. [D] . Roidl, Benedikt. 2008

机译：多级涡轮机械叶片的空气动力学逆设计。
6. Very low energy cross sections for collision-induced rotational relaxation of I2 seeded in a supersonic free jet [O] . James Tusa, Mark Sulkes, Stuart A. Rice 1980

机译：超音速自由射流中I2的碰撞诱导的I2旋转弛豫的能量截面非常低
7. Turbulences of the supersonic gas flow during cold spraying and their negative effects: A DNS CFD analysis coupled with experimental observation and laser impulse high-speed shadowgraphs of the particles in-flight flow [O] . R.N. Raoelison, L.L Koithara, S. Costil, 2020

机译：冷喷涂过程中超声波气流的湍流及其负面影响：具有实验观察和激光脉冲的DNS CFD分析和飞行中的粒子的高速影子图
8. Analytical Investigation of Supersonic Turbomachinery Blading. 2 - Analysis of Impulse Turbine-Blade Sections [R] . Goldman, L. J. 1968

机译：超音速涡轮机叶片的分析研究。 2 - 脉冲涡轮叶片截面的分析

Analytical investigation of supersonic turbomachinery blading. 2 - Analysis of impulse turbine-blade sections

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