Computational and physical aspects of vortex breakdown on delta wings-Reference-Cited by-同舟云学术

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Computational and physical aspects of vortex breakdown on delta wings

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Visbal M

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-585

Reference118 articles.

1. Bannink, W. J., Houtman, E. M. and Ottochian, S. P. "Investigation of the Vortex Flow over a Sharp Edged Delta Wing in the Transonic Regime," Report LR-594, Faculty of Aerospace Engineering, Delft University of Technology, October 1989.

Cited by 53 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. Numerical Simulation of Effect of Vectoring Jets on the Vortex Dominated Flow Over a Delta Wing at High Angles of Attack;AIAA SCITECH 2024 Forum;2024-01-04

2. Revisit of the Breakdown Characteristics of the Leading-Edge Separation Vortices over a Delta Wing;AIAA SCITECH 2023 Forum;2023-01-19

3. Hybrid RANS-LES Simulation of Vortex-Dominant Flow Over a Delta Wing at High Angles of Attack;AIAA SCITECH 2022 Forum;2022-01-03

4. Investigation of the effects of angle of attack and tail deflection angle on the controlling tail flow field;Aerospace Systems;2020-10-19

5. Vortex Flow and Aerodynamic Performance of a Reverse Delta Wing;AIAA Journal;2020-02

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