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Water tunnel flow visualization studies of a Canard-Configured X-31A- like fighter aircraft model

机译：Canard配置的X-31A型战斗机模型的水隧道流动可视化研究

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Approved for public release, distribution unlimited

机译：批准公开发行，发行不限

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作者
Kwon Hui Man;
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年度 2013
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原文格式 PDF
正文语种 en_US
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专利

1. 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
2. Measurement of flow-induced pressures on the surface of a model in a flow visualization water tunnel [J] . Erm LP. Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2003,第6期

机译：在水流可视化水洞中测量模型表面的水流压力
3. Sukhoi SU-47 Berkut and Eurofighter Typhoon Models Flow Visualization and Performance Investigation Using GAMA Water Tunnel [J] . Sutrisno ., Febryanto Nugroho, Yogi Adi Pratama, Modern Applied Science . 2019,第2期

机译：Sukhoi SU-47 Berkut和Eurofighter台风模型使用GAMA输水管道进行流量可视化和性能研究
4. Water Tunnel Flow Visualization Due to Canard Deflection Effect on Aircraft to Improve Stall Delay Performance [C] . Setyawan Bekti Wibowo, Sutrisno, Tri Agung Rohmat International Conference on Science and Technology - Computer . 2018

机译：鸭翼偏转效应对飞机的水隧道流动可视化，以改善失速延迟性能
5. Reconfigurable flight control for high angle of attack fighter aircraft, with wind tunnel study [D] . Siddiqui, Bilal Ahmed 2010

机译：高攻角战斗机的可重构飞行控制，带有风洞研究
6. Visualization Study of Oil-in-Water-in-Oil (O/W/O) Double Emulsion Formation in a Simple and Robust Co-Flowing Microfluidic Device [O] . Pengfei Lu, Liangyu Wu, Xiangdong Liu 2017

机译：简单且稳健的共流微流控装置中油包水油（O / W / O）双乳液形成的可视化研究
7. Flow visualization studies of a sideslipping, canard-configured X-31A-like fighter aircraft model. [O] . Kim Chang Ho. 1991

机译：侧滑，鸭式配置的X-31A型战斗机模型的流动可视化研究。

Water tunnel flow visualization studies of a Canard-Configured X-31A- like fighter aircraft model

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