Large-scale viscous simulation of laminar vortex flow over a delta wing

Author:

Rizzi Arthur1,Muller Bernhard1

Affiliation:

1. Aeronautical Research Institute of Sweden, Bromma, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 17 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. Effects of pitch, yaw, and roll on delta wing skin friction topology;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2015-07-14

2. Development and Verification of a Flow Model of Conical Vortices on Saddle Roofs;Journal of Engineering Mechanics;2015-03

3. Improvement and validation of a flow model for conical vortices;Wind and Structures;2014-08-25

4. Skin friction fields on delta wings;Experiments in Fluids;2009-05-29

5. A model of roof-top surface pressures produced by conical vortices : Model development;Wind and Structures;2001-06-25

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