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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : aerodynamic characteristics in sideslip of a large-scale model having a 63 degree swept-back vertical tail

机译：使用机翼后掠63度的机翼 - 机身组合的空气动力学研究：具有63度后掠垂直尾翼的大型模型的侧滑中的空气动力学特性

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Mccormack, Gerald M;
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年度 1949
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. Reynolds number effects on flow characteristics and aerodynamic performances of a swept-back wing [J] . Shun C. Yen, Lung-C. Huang Aerospace science and technology . 2011,第3期

机译：雷诺数对后掠机翼流动特性和空气动力性能的影响
2. Investigation of wind tunnel wall effect and wing-fuselage interference regarding the prediction of wing aerodynamics and its influence on the horizontal tail [J] . Hoang Ngoc T. B., Bui Binh V. Journal of Mechanical Science and Technology . 2019,第6期

机译：关于翼空气动力学预测及其对水平尾部的影响的风洞壁效应和机翼机身干扰
3. Aerodynamic Performance and Surface Flow Structures of Leading-Edge Tubercled Tapered Swept-Back Wings [J] . Wei Zhaoyu, New T. H., Cui Y. D. AIAA Journal . 2018,第1期

机译：前缘锥形渐缩后掠翼的气动性能和表面流动结构
4. CFD Analysis of Aerodynamic Characteristics of Low Reynolds Number High Lift Airfoils FX 63-137 and Selig S1223 by deploying Gurney Flaps [C] . Absar Ahmed Khan, Mirza Wasif Saeed Accelerating Space Commerce, Exploration, and New Discocery Conference . 2020

机译：通过部署Gurney PLAPS的低雷诺数高升降机翼型FX 63-137和SELIG S1223的空气动力学特性的CFD分析
5. Rapid Prediction of Post-Stall Aerodynamic Characteristics of Aircraft with Swept Wings [D] . Hosangadi, Pranav. 2019

机译：用扫翅膀的飞机后空气动力学特性的快速预测
6. Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps [O] . Rinoie K. 1996

机译：带有涡流襟翼的60度圆形前缘三角翼的低速空气动力学特性

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : aerodynamic characteristics in sideslip of a large-scale model having a 63 degree swept-back vertical tail

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