Computational investigation of vortex structure and breakdown over a delta wing at supersonic pitching maneuver

Author:

Hadidoolabi M.,Ansarian H.ORCID

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Reference31 articles.

1. Gursul I, Gordnier R, Visbal M (2005) Unsteady aerodynamics of nonslender delta wings. Prog Aerosp Sci 41(7):515–557

2. Gursul I (2004) Recent developments in delta wing aerodynamics. Aeronaut J 108(1087):437–452

3. Rockwell D (1993) Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts issues. In: 31st aerospace science meeting and exhibit, Reno, Nevada, Paper No. 93-0550

4. Visbal MR (1993) Computational and physical aspects of vortex breakdown on delta wings. In: 33rd aerospace science meeting and exhibit, Reno, Nevada, paper no. 95-0585

5. Maltby RL, Engler PB, Keating RFA (1963) Some exploratory measurements of leading-edge vortex positions on a delta wing oscillating in heave. Aeronautical Research Council, Research and Memorandum, No. 3410, London

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