Experimental and Numerical Investigation of Transition in a Separated Shear Layer

机译：分离剪切层中转变的实验和数值研究

获取原文

获取原文并翻译 | 示例

页面导航

摘要
著录项
相似文献
相关主题

摘要

Laminar boundary layer separation occurs on the upper surface of the NACA 0025 airfoil for Re_c=15x10~4 and Re_c=10x10~4 and at angles of attack of 0°, 5° and 10°. The separated boundary layer undergoes transition and can reattach to the airfoil surface. The comparison of numerical and experimental results suggest mat linear stability theory can be employed to describe the initial stage of the separated shear layer transition on an airfoil at low Reynolds numbers.

机译：当Re_c = 15x10〜4和Re_c = 10x10〜4且迎角为0°，5°和10°时，层边界层分离发生在NACA 0025机翼的上表面。分离的边界层经历过渡并且可以重新附着到机翼表面。数值和实验结果的比较表明，垫层线性稳定性理论可用于描述低雷诺数下机翼上分离剪切层过渡的初始阶段。

著录项

来源
《Canadian Congress of Applied Mechanics(CANCAM 2005); 20050530-0602; Montreal(CA)》|2005年|P.251-252|共2页
会议地点 Montreal(CA)
作者
S. Yarusevych; J.G. Kawall; P.E. Sullivan;
展开▼
作者单位

Department of Mechanical and Industrial Engineering, University of Toronto, Toronto, Ontario, Canada, M5S 3G8;

展开▼
会议组织
原文格式 PDF
正文语种 eng
中图分类机械制造工艺;
关键词

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. Numerical and Experimental Modelling of Transition in a Separated Boundary Layer on the NACA63A421 Airfoil [J] . Miroslav ?URI?, Luká? POPELKA, Jaromír P?íHODA, Transactions of the VSB - Technical University of Ostrava: Mechanical Series . 2010,第3期

机译：NACA63A421机翼上分离边界层过渡的数值和实验建模
4. Experimental and Numerical Investigation of Transition in a Separated Shear Layer [C] . S. Yarusevych, J.G. Kawall, P.E. Sullivan Canadian Congress of Applied Mechanics . 2005

机译：分离剪切层中过渡的实验性和数值研究
5. Prediction of transition for attached and separated shear layers in turbomachinery. [D] . Langtry, Robin Blair. 2003

机译：涡轮机械中附着和分离的剪切层的过渡预测。
6. Experimental and Numerical Investigation on the Perforation Resistance of Double-Layered Metal Shield under High-Velocity Impact of Armor-Piercing Projectiles [O] . Riccardo Scazzosi, Marco Giglio, Andrea Manes 2021

机译：双层金属屏蔽在盔甲孔径射孔高速冲击下的孔隙性抗性的实验性和数值研究
7. Numerical Investigations of Instability and Transition in Attached and Separated Shear Layers [O] . Joshua Brinkerhoff -1

机译：附着和分离剪力层中不稳定性和过渡的数值研究
8. Transition to Turbulence in the Separated Shear Layers of Yawed Circular Cylinders [R] . Jordan, S. A. 2010

机译：偏航圆柱分离剪切层向湍流过渡

Experimental and Numerical Investigation of Transition in a Separated Shear Layer

摘要

著录项

相似文献

相关主题

期刊订阅