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A study of the flow field behind the triangular horizontal tail of a canard airplane at approximately the vertical-tail location by means of a tuft grid

机译：利用簇绒网格研究大约垂直尾部位置的鸭式飞机三角形水平尾翼后面的流场

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Johnson, Joseph L , Jr;
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年度 1952
页码 1-21
总页数 21
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. 安装和不安装垂直嵌板的鸭式飞机横向稳定性研究 [J] . 殷熙凤, 黄明信, 朴郁济, 南京航空航天大学学报（英文版） . 2003,第002期
2. Mitigating horizontal divergence "checker-board" oscillations on unstructured triangular C-grids for nonlinear hydrostatic and nonhydrostatic flows [J] . Wolfram P.J., Fringer O.B. Ocean modelling . 2013,第Null期

机译：缓解非线性静水和非静水流动的非结构三角C网格上的水平发散“棋盘”振荡
3. Photochemical grid model performance with varying horizontal grid resolution and sub-grid plume treatment for the Martins Creek near-field SO_2 study [J] . Kirk R. Baker, Andy Hawkins, James T. Kelly Atmospheric environment . 2014,第deca期

机译：Martins Creek近场SO_2研究中不同水平网格分辨率和亚网格羽化处理的光化学网格模型性能
4. EFFECT OF THE HORIZONTAL CANARD OF THE SHARP-EDGED FOREBODY OF THE MANEUVERABLE AIRCRAFT MODEL ON THE VORTEX FLOW STRUCTURE [J] . Konstantin Anatolievich Osipov TsAGI science journal . 2019,第1期

机译：操纵飞机模型前缘锋面水平翼对涡流结构的影响
5. Flow Fields Around The Tails Of Aircraft With Outboard Horizontal Stabilizers [C] . J. Kentfield, B. Wong AIAA Aerospace Sciences Meeting and Exhibit . 2006

机译：带有舷外水平稳定器的飞机机尾周围的流场
6. A theoretical and numerical study of the use of grid embedded axial magnetic fields to reduce charge exchange ion induced grid erosion in electrostatic ion thrusters. [D] . Claypool, Ian R. 2007

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7. A Case Study of Connection Between Ground Magnetic Field Perturbations and Tail Current Sheet Bursty Flows at X = −60 RE [O] . Chih-Ping Wang, Xiaoyan Xing, Yi-Hsin Liu, -1

机译：X = −60 RE时地磁场扰动与尾电流表爆流之间的联系的案例研究
8. Design loads for horizontal tail surfaces for airplanes [O] . Fahrney Delmer Stater, Gilbert Ward Carr 1925

机译：飞机水平尾翼表面的设计载荷

A study of the flow field behind the triangular horizontal tail of a canard airplane at approximately the vertical-tail location by means of a tuft grid

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