Aerodynamic Performance and Surface Flow Structures of Leading-Edge Tubercled Tapered Swept-Back Wings

Wei Zhaoyu; New T. H.; Cui Y. D.

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Aerodynamic Performance and Surface Flow Structures of Leading-Edge Tubercled Tapered Swept-Back Wings

机译：前缘锥形渐缩后掠翼的气动性能和表面流动结构

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来源
《AIAA Journal》 |2018年第1期|423-431|共9页
作者
Wei Zhaoyu; New T. H.; Cui Y. D.;
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作者单位

Shanghai Jiao Tong Univ, Inst Oceanog, 800 Dongchuan Rd, Shanghai 200240, Peoples R China;

Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore;

Natl Univ Singapore, Temasek Labs, Engn Dr 1, Singapore 117411, Singapore;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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1. Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number [J] . Wei Zhaoyu, New T. H., Lian Lian, Ocean Engineering . 2019,第JUNa1期

机译：前缘结节在非常低的雷诺数下延迟了锥形后掠式机翼的气流分离
2. Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number [J] . Wei Zhaoyu, New T. H., Lian Lian, Ocean Engineering . 2019,第Juna1期

机译：前沿结节在非常低的雷诺数下锥形扫反翼延迟流分离
3. Enhancing the hydrodynamic performance of a tapered swept-back wing through leading-edge tubercles [J] . Wei Zhaoyu, Lian Lian, Zhong Yisen Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2018,第6期

机译：通过前缘结节增强锥形扫翼翼的流体动力学性能
4. Controlling Secondary-Flow Structure by Leading-Edge Airfoil Fillet and Inlet Swirl to Reduce Aerodynamic Loss and Surface Heat Transfer [C] . T. I-P. Shih, Y.-L. Lin ASME (American Society of Mechanical Engineers) Turbo Expo 2002: Heat Transfer Manufacturing Materials and Metallurgy . 2002

机译：通过前缘翼型角和进气旋流控制次级流结构，以减少空气动力损失和表面传热
5. The effect of biologically-inspired, passive, leading-edge tubercles on static and flapping wing flight. [D] . Cho, Byong-Chun Ben. 2007

机译：受生物启发的被动前沿结节对机翼和襟翼飞行的影响。
6. Leading-edge vortices over swept-back wings with varying sweep geometries [O] . William B. Lambert, Mathew J. Stanek, Roi Gurka, 2019

机译：后掠翼上的前缘涡旋具有不同的掠掠几何形状
7. Experimental Investigations on Leading-Edge Vortex Structures for Flow over Non-Slender Delta Wings ∗ [O] . 2007

机译：非细长三角翼上流动前缘涡结构的实验研究*

Aerodynamic Performance and Surface Flow Structures of Leading-Edge Tubercled Tapered Swept-Back Wings

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