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Flow visualization of the effect of pitch rate on the vortex development on the scale model of a F-18 fighter aircraft.

机译：F-18战斗机比例模型上的俯仰率对涡旋发展影响的流动可视化。

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http://archive.org/details/flowvisualizatio00park

机译：HTTP://archive.org/details/flow visual i杂题哦00park

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作者
Park Sung-Nam;
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年度 1989
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原文格式 PDF
正文语种 en_US
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专利

1. The Flow Visualization CFD Studies of the Fuselage and Rolled-up Vortex Effects of the Chengdu J-10-like Fighter Canard [J] . Sutrisno ., Tri Agung Rochmat, Setyawan Bekti Wibowo, Modern Applied Science . 2018,第2期

机译：成都J-10-型战斗机机壳和涡旋效应的流动可视化CFD研究
2. Visualization of vortex flow patterns with a uniformly perforated showerhead in a model lamp heat, single-wafer thermal processor [J] . Cheng TC, Lin TF, Yang JY, Chemical vapor deposition: CVD . 2007,第8期

机译：在模型灯加热单晶片热处理器中使用均匀穿孔的喷头可视化涡流模式
3. Performance Analysis and Visualization of Canard and Fuselage Effects on Flow Patterns around a Straight-Body-Type-Fuselage (SBTF) Fighter Models with Experimental Method in Water Tunnel [J] . Sutrisno ., Firdaus RS, Zainuri A, Modern Applied Science . 2018,第10期

机译：水上隧道实验中鸭身和机身对直线型战斗机（SBTF）战斗机周围流型的性能分析和可视化
4. Separated Flow Discrete Vortex Model for Nano- Scale Hovering Flapping Wings [C] . P. Zdunich AIAA Applied Aerodynamics Conference . 2008

机译：纳米级悬停扑翼的分离流动离散涡模型
5. The development of an enhanced stability compensation design concept for a statically unstable fighter aircraft with a large stable pitching moment break at high angles of attack [D] . Lu, Cheng-Huei. 1989

机译：针对在高攻角下具有较大的稳定俯仰力矩中断的静态不稳定战斗机，增强了稳定性补偿设计概念的发展
6. Assessment of stretched vortex subgrid-scale models for LES of incompressible inhomogeneous turbulent flow [O] . Dinesh A. Shetty, Steven H. Frankel -1

机译：不可压缩非均匀湍流LES的拉伸涡流亚网格尺度模型的评估
7. A Flow Visualization Study of LEX Generated Vortices on a Scale Model of a F/A-18 Fighter Aircraft at High Angles of Attack [O] . Cavazos Odilon V. Jr. 1990

机译：F / A-18战斗机在高攻角比例模型上LEX产生涡流的流动可视化研究

Flow visualization of the effect of pitch rate on the vortex development on the scale model of a F-18 fighter aircraft.

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