首页> 外文OA文献 >Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections

【2h】

Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections

机译：用尾瓣旋转偏转的各种攻击角度分离剪切层的实验研究

代理获取

本网站仅为用户提供外文OA文献查询和代理获取服务，本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文，但由于OA文献来源多样且变更频繁，仍可能出现获取不到、文献不完整或与标题不符等情况，如果获取不到我们将提供退款服务。请知悉。

页面导航

著录项
引文网络
相似文献
相关主题

著录项

作者
K ANAND; S SARKAR;
展开▼
作者单位

展开▼
年度 2015
总页数
原文格式 PDF
正文语种
中图分类

相似文献

外文文献
中文文献
专利

1. Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections [J] . Anand K., Sarkar S. Sadhana: Academy Proceedings in Engineering Science . 2015,第3期

机译：从前缘分离的剪切层的实验研究
2. Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections [J] . K Anand, S Sarkar Sadhana . 2015,第3期

机译：从前缘分离剪切层的实验研究
3. Investigation of the effects of angle of attack and tail deflection angle on the controlling tail flow field [J] . Ali Mokhtari, Azadeh Shahrian, Pooya Javadpoor Langroodi, Aerospace Systems . 2020,第4期

机译：攻击角度对控制尾流场的影响研究
4. Experimental Investigation of Separated Shear Layer over a Flat Plate for Various Angles of Attack and Tail Flap Deflections [C] . K. Anand, S. Sarkar ASME turbo expo: turbine technical conference and exposition . 2014

机译：平板上分开的剪切层对各种迎角和尾翼挠度的实验研究
5. Effects of asymmetric leading edge flap deflection on delta wings. [D] . Ize, Carlos. 1998

机译：不对称的前缘襟翼偏斜对三角翼的影响。
6. Moth tails divert bat attack: Evolution of acoustic deflection [O] . Jesse R. Barber, Brian C. Leavell, Adam L. Keener, 2015

机译：蛾尾转移了蝙蝠的攻击：声音偏转的演变
7. Correction: The Effects of Leading Edge Flap and Trailing Edge Flaperon Deflections on Horizontal Tail Optimization [O] . Fazil S. Gomec, Emre C. Unver, Mehmet Z. Arisoy 2020

机译：校正：前沿襟翼和后缘FLAPERON偏转对水平尾优化的影响
8. Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft [R] . White, E. R. 1982

机译：机翼前缘改进对T型尾翼低翼通用航空飞机大迎角特性影响的风洞研究

Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections

著录项

引文网络

相似文献

相关主题

期刊订阅