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Effect of jet velocity and axial location of nozzle exit on the performance of a twin-jet afterbody model at Mach numbers up to 2.2

机译：射流速度和喷嘴出口轴向位置对马赫数为2.2的双喷射后体模型性能的影响

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摘要

Jet velocity and axial location of nozzle exit on performance of twin-jet afterbody model

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作者
Berrier, B. L.; Wood, F. H., Jr.;
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年度 1969
页码 1-80
总页数 80
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ANGLE OF ATTACK; JET ENGINES; NOZZLE DESIGN; PERFORMANCE TESTS; WIND TUNNEL MODELS; AIRCRAFT MODELS; GRAPHS (CHARTS); NOZZLE GEOMETRY;

机译：攻击角度;喷气发动机;喷嘴设计;性能测试;风洞模型;飞机模型;图表（图表）;喷嘴几何;

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1. Impact of tab location relative to the nozzle exit on the shock structure of a supersonic jet [J] . Kumar P. Arun, Aileni Manideep, Rathakrishnan E. Physics of fluids . 2019,第7期

机译：突变位置相对于喷嘴出口的影响超声波射流的冲击结构
2. Effect of Nozzle Exit Turbulence on the Column Trajectory and Breakup Location of a Transverse Liquid Jet in a Gaseous Flow [J] . Broumand Mohsen, Rigby Graham, Birouk Madjid Flow, turbulence and combustion . 2017,第1期

机译：喷嘴出口湍流对气流横液射流柱轨迹和分解位置的影响
3. On the spectra of nozzle-exit velocity disturbances in initially nominally turbulent, transitional jets [J] . Bogey C., Marsden O., Bailly C. Physics of fluids . 2011,第9期

机译：在最初名义上湍流的过渡射流中喷嘴出口速度扰动的频谱
4. The Effect of Laminar Nozzle Exit Boundary Layer Thickness on a Mach 1.3 Jet With and Without Control [C] . Rachelle L. Speth, Datta V. Gaitonde AIAA fluid dynamics conference and exhibit . 2012

机译：层流喷嘴出口边界层厚度对有和无控制的1.3马赫射流的影响
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. A Study on the Influence of the Nozzle Lead Angle on the Performance of Liquid Metal Electromagnetic Micro-Jetting [O] . Zhiwei Luo, Gaofeng Zheng, Lingyun Wang 2016

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7. Estimation of afterbody drag with jet temperature effects for the afterbody-nozzle configuration of a combat aircraft [O] . Mathur NB 1999

机译：战斗机后喷嘴结构对射流温度影响的后阻力的估计
8. Effect of Jet Velocity and Axial Location of Nozzle Exit on the Performance of a Twin-Jet Afterbody Model at Mach Numbers Up to 2.2 [R] . Berrier, B. L., Wood, F. H. 1969

机译：喷嘴出口的射流速度和轴向位置对马赫数高达2.2的双射流后体模型性能的影响

Effect of jet velocity and axial location of nozzle exit on the performance of a twin-jet afterbody model at Mach numbers up to 2.2

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