Evolution of vortical structures in the shear-layer of delta wings-Reference-Cited by-同舟云学术

Evolution of vortical structures in the shear-layer of delta wings

Published:1994-06-20 Issue: Volume: Page:
ISSN:
Container-title:Fluid Dynamics Conference
language:
Short-container-title:

Author:

Washburn Anthony¹,Visser Kenneth²

Affiliation:

1. VIGYAN, Inc., Hampton, VA

2. National Research Council, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2317

Reference16 articles.

1. Reynolds, G. A. and Ahtahi, "Three-Dimensional Vortex Development, Breakdown, and Control", AIAA89-0998.

2. Payne, F. M. "The Structure of Leading Edge Vortex Flows Including Vortex Breakdown", Ph.D. Dissertation,Department of Acrospace and Mechanical Engineering, Universityof Norte Dame, Notre Dame, IN,May 1987. 6 Washburn, A. E. "Effects of External Influences on Subsonic Delta Wing Vortices", AIAA-92-4033, July, 1992. 7 Verhaagen, N. G.; Meader, J. P.; and Verhelst, J. M. "Boundary Layer Effects on the Flow of a Leading Edge Vortex". AIAA-93-3463-CP,Aug. 1993.

Cited by 25 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. Vortex dynamics of axisymmetric cones at high angles of attack;Theoretical and Computational Fluid Dynamics;2023-05-04

2. Study of the transient flow structures generated by a pulsed nanosecond plasma actuator on a delta wing;Physics of Fluids;2022-10

3. A Focused Study into the Prediction of Vortex Formation about Generic Missile and Combat Aircraft Airframes;AIAA SCITECH 2022 Forum;2022-01-03

4. Flow Over the Tip Region of a Flexible Cantilever Wing With the Effect of Angle of Attack;Journal of Fluids Engineering;2019-03-18

5. Zonal Detached-Eddy Simulation of Separated Flow Around a Finite-Span Wing;AIAA Journal;2015-11