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Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane tapered wing of aspect ratio 3.1 with 3-percent-thick, biconvex section

机译：低纵横比机翼在亚音速和超音速下的升力，阻力和俯仰力矩：长宽比3.1的平面锥形机翼，厚度为3％，双凸面截面

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Reese, David E; Phelps, E Ray;
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年度 1951
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Lift and Drag of Non-conventional Wings at Subsonic Speeds and Zero Angle of Attack - An Experimental Investigation [J] . Abdulkareem Shafiq Mahdi Al-Obaidi, Ting Chern Wei MATEC Web of Conferences . 2018,第1期

机译：非常规机翼在亚音速和零迎角下的升起和阻力-实验研究
2. On the mechanism of high-incidence lift generation for steadily translating low-aspect-ratio wings [J] . DeVoria Adam C., Mohseni Kamran Journal of Fluid Mechanics . 2017,第期

机译：高发升升力施工中低纵横比翅膀的机理
3. Small Disturbance Navier-Stokes Computations for Low-Aspect-Ratio Wing Pitching Oscillations [J] . Alexander Pechloff, Boris Laschka Journal of Aircraft . 2010,第3期

机译：低纵横比机翼俯仰振荡的小扰动Navier-Stokes计算
4. Lift, drag and pitching moment performances of different wing profiles for MAV wings [C] . N I Ismail, H Yusoff, H Sharudin, International Conference on Nanomaterials: Science, Engineering and Technology . 2020

机译：用于MAV翅膀的不同机翼型材的升降机，拖动和投球时刻表演
5. Study of belly-flaps to enhance lift and pitching moment coefficient of a Blended-Wing-Body airplane in landing and takeoff configuration. [D] . Staelens, Yann Daniel. 2007

机译：研究腹部襟翼，以提高降落和起飞配置下的混合机翼机身飞机的升力和俯仰力矩系数。
6. A vortex model for forces and moments on low-aspect-ratio wings in side-slip with experimental validation [O] . Adam C. DeVoria, Kamran Mohseni -1

机译：侧滑低纵横比机翼上力和力矩的涡流模型并通过实验验证
7. Extension to the Panel Code NALSOP0509 to Include Designudof Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment [O] . Desai SS, Narayana CL, Rangarajan R 1985

机译：面板代码NALSOP0509的扩展以包括Design ud给定升力和俯仰力矩下机翼结构的最小感生阻力

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane tapered wing of aspect ratio 3.1 with 3-percent-thick, biconvex section

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