Delayed detached-eddy simulation of vortex breakdown over a 70° delta wing

Author:

Son Mi So,Sa Jeong Hwan,Park Soo Hyung,Byun Yung Hwan,Cho Kum Won

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference35 articles.

1. D. H. Peckhom and S. A. Atkinson, Preliminary results of low speed wind tunnel tests on a gothic wing of aspect ratio 1.0, ARC. TR. No. 508 (1960).

2. R. C. Nelson and A. Pelletier, The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers, Elsevier Science Ltd., USA (2003) 185–248.

3. A. Mitchell, P. Molton, D. Barberis and J. Délery, Characterization of vortex breakdown by flow field and surface measurements, 38th Aerospace Sciences Meeting & Exhibit, Reno, NV, USA (2000).

4. S. Agrawal, R. M. Barnett and B. A. Robinson, Numerical investigation of vortex breakdown on a delta wing, AIAA Journal, 30 (3) (1992) 584–591.

5. J. Rom, High angle of attack aerodynamics: Subsonic, transonic, and supersonic flows, Springer-Verlag, New York, USA (1992).

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