Shock control on a swept wing

Jochen Birkemeyer; Henning Rosemann; Egon Stanewsky

首页> 外文期刊>Aerospace science and technology >Shock control on a swept wing

【24h】

Shock control on a swept wing

机译：后掠机翼的减震控制

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

Shock and boundary layer control by contour bumps and local boundary layer suction have been investigated experimentally and numerically on a transonic swept wing. Additional 2-D numerical investigations were performed for the airfoil, corresponding to the wing. The investigations were primarily stimulated by the question concerned with the influence of sweep on The bump effectiveness. This influence has been found to be rather small; the drag reduction by the bump is Slightly lower for the swept wing than for the airfoil.

机译：在跨音速扫掠机翼上，通过实验和数值研究了轮廓波和局部边界层吸力对冲击和边界层的控制。对翼型（对应于机翼）进行了附加的二维数值研究。有关扫频对颠簸效果的影响主要是激发了调查工作。已经发现这种影响很小。颠簸产生的阻力减少率对于后掠机翼比机翼略低。

著录项

来源
《Aerospace science and technology》 |2000年第3期|p.147-156|共10页
作者
Jochen Birkemeyer; Henning Rosemann; Egon Stanewsky;
展开▼
作者单位

展开▼
收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空、航天;
关键词
transonic aerodynamics; swept wing; shock and boundary layer control;

机译：跨音速空气动力学后掠翼冲击和边界层控制;

相似文献

外文文献
中文文献
专利

1. Design of a Sliding Mode Control for Wing Rock Suppression in Highly-Swept Wing Aircraft [J] . Giorgio Guglieri, Daniele Sartori International Journal of Aerospace Sciences . 2013,第1期

机译：大扫掠机翼飞机压制机翼的滑模控制设计
2. Numerical Simulation of Shock-Stall Flutter of a High-Aspect-Ratio Forward-Swept Wing [J] . Koji Isogai Transactions of the Japan society for aeronautical and space sciences . 2013,第5期

机译：高纵横比前掠机翼减振颤振的数值模拟
3. Stability and Control Investigations of Generic 53 Degree Swept Wing with Control Surfaces [J] . Schuette Andreas, Huber Kerstin C., Frink Neal T., Journal of Aircraft . 2018,第2期

机译：带有控制面的通用53度后掠翼的稳定性和控制研究
4. Investigations on Shock Control Bumps for Infinite Swept Wings [C] . M. Kutzbach, T. Lutz, S. Wagner 34th AIAA Fluid Dynamics Conference ; 2nd AIAA Flow Control Conference ; 35th AIAA Plasmadynamics and Lasers Conference ; 37th AIAA Thermophysics Conference . 2004

机译：无限扫掠机翼的冲击控制凸点研究
5. Control of a swept wing tailless aircraft through wing morphing . [D] . Guiler, Richard W. 2007

机译：通过机翼变形控制掠过机翼无尾飞机。
6. Leading-edge vortices over swept-back wings with varying sweep geometries [O] . William B. Lambert, Mathew J. Stanek, Roi Gurka, 2019

机译：后掠翼上的前缘涡旋具有不同的掠掠几何形状
7. Numerical Simulation of Shock-Stall Flutter of a High-Aspect-Ratio Forward-Swept Wing [O] . Koji ISOGAI 2013

机译：高纵横比前扫翼的冲击扑颤的数值模拟
8. Hinge moment and effectiveness of an unswept constant-chord control and an overhang-balanced, swept hinge-line control on an 80 degree swept pointed wing at Mach numbers from 0.75 to 1.96 [R] . Guy, Lawrence D 1956

机译：铰接力矩和有效性的未扫描恒定弦控制和悬臂平衡，扫过铰链线控制在80度扫描尖翼，马赫数从0.75到1.96

Shock control on a swept wing

摘要

著录项

相似文献

相关主题

期刊订阅