Attachment-Line Flow on an Infinite Swept Wing
Author:
Affiliation:
1. Douglas Aircraft Company, Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference1 articles.
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Lie derivatives of fundamental surface quantities in incompressible viscous flows;Physics of Fluids;2023-05-01
2. Structures of Skin Friction, Surface Pressure, and Boundary Enstrophy Flux in Attachment-Line Flow;Journal of Fluids Engineering;2019-09-19
3. Re-orienting the Turbulent flow over an Inclined Cylinder of Finite Aspect ratio;2018 Flow Control Conference;2018-06-24
4. Quasi-One-Dimensional and Quasi-Two- Dimensional Flows;Three-Dimensional Attached Viscous Flow;2014
5. Transition flight experiments on a swept wing with suction;20th Fluid Dynamics, Plasma Dynamics and Lasers Conference;1989-06-12
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