Numerical investigation into vortical flow about a delta-wing configuration up to incidences at which vortex breakdown occurs in experiment-Reference-Cited by-同舟云学术

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Numerical investigation into vortical flow about a delta-wing configuration up to incidences at which vortex breakdown occurs in experiment

Published:1994-01-10 Issue: Volume: Page:
ISSN:
Container-title:32nd Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

van den Berg J.¹,Hoeijmakers H.²,Brandsma F.¹

Affiliation:

1. National Aerospace Lab., Amsterdam, Netherlands

2. Delft Univ. of Technology, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-621

Reference23 articles.

1. [Z] Long 0,J.M.A.: The Role of Numerical Dissipation on the Computational Euler-Equations Solutionsfor Vortical Flows. AIAA Paper 89-2232, (1989)

2. Hitze 1,S.M.:Wing Vorler-Flows up into Vortel: Breakdown. A Nurn.erical Simulation. AIAA Paper 89-2232

Cited by 3 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. Revisit of the Breakdown Characteristics of the Leading-Edge Separation Vortices over a Delta Wing;AIAA SCITECH 2023 Forum;2023-01-19

2. Compressibility effects on vortex breakdown onset above a 75-degree sweep delta wing;Journal of Aircraft;1995-09

3. Computation of the flow about a F16-like configuration for several flow conditions;13th Applied Aerodynamics Conference;1995-06-19

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