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Computational Flow Analysis and Drag Coefficient Research for Angle of Attack in Slocum Underwater Glider

机译：斜坡水下滑翔机攻角的计算流动分析与拖曳系数研究

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Jeong-Woo Park; Jung-Woo Lee; Young-Ho Choi; Kap-Ho Seo; Jin-Ho Suh; Jong-Jin Park;
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年度 2016
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1. Slocum Gliders as Relocatable Waveriders of Opportunity Increasing Underwater Glider Sensing Capabilities With Smart Payloads [J] . Garau Bartolome, Alvarez Alberto Sea Technology: Worldwide Information Leader for Marine Business, Science & Engineering . 2016,第6期

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2. Computational drag and lift for a transonic flow past a SOCBT projectile with and without porous surface at angles of attack [J] . Jih-Lan HSIUNG, Shing-Chung ONN, Nai-Chung YANG JSME International Journal. Series B . 1997,第1期

机译：跨音速流经过SOCBT子弹时的有声和无声表面的计算阻力和升力
3. An investigation of free surface effects on drag and lift coefficients of an autonomous underwater vehicle (AUV) using computational and experimental fluid dynamics methods [J] . Mansoorzadeh Sh., Javanmard E. Journal of Fluids and Structures . 2014,第Null期

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4. The analysis of viscous resistance towards various configuration of angle of attack and chord length of the foil towards the creation of the bubble on drag reduction of the ship on winged air induction pipe using computational fluid dynamics [C] . Yanuar, Muhammad Alief, M. Akbar, International Tropical Renewable Energy Conference . 2020

机译：用计算流体动力学将箔攻击角度和箔角度的各种配置的分析与箔的各种配置与箔造成船舶减阻
5. COMPUTATION OF THE INVISCID SUPERSONIC FLOW ABOUT CONES AT LARGE ANGLES OF ATTACK BY A FLOATING DISCONTINUITY APPROACH. [D] . DAYWITT, JAMES EDWARD. 1977

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6. From bead to rod: Comparison of theories by measuring translational drag coefficients of micron-sized magnetic bead-chains in Stokes flow [O] . Kaiyuan Yang, Chen Lu, Xiaodan Zhao, 2011

机译：从磁珠到棒：通过测量斯托克斯流中微米大小的磁珠链的平移阻力系数进行理论比较
7. Computational Drag and Lift for a Transonic Flow past a SOCBT Projectile with and without Porous Surface at Angles of Attack. [O] . Jih-Lan HSIUNG, Shing-Chung ONN, Nai-Chung YANG 1997

机译：计算阻力和升降横向流过SOCBT射弹，在攻击角度的角度下没有多孔表面。
8. An Approximate Solution of Additive-Drag Coefficient and Mass-Flow Ratio for Inlets Utilizing Right Circular Cones at Zero Angle of Attack [R] . Mascitti, V. R. 1969

机译：零攻角下利用右圆锥进气道阻力系数和质量流量比的近似解

Computational Flow Analysis and Drag Coefficient Research for Angle of Attack in Slocum Underwater Glider

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