The dynamic vortical flow behaviour on a coplanar canard configuration during large-amplitude-pitching

Author:

Chen Qingmin,Hu Tianxiang,Liu Peiqing,Qu Qiulin,Guo Hao,Akkermans Rinie A.D.

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

1. Predictions of vortex-lift characteristics by a leading-edge suction analogy;Polhamus;J. Aircr.,1971

2. Basic low speed aerodynamics of short-coupled canard configuration of small aspect ratio;Behrbohm;SAAB,1965

3. A scaling for vortex formation on swept and unswept pitching wings;Onoue;J. Fluid Mech.,2017

4. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers;Nelson;Prog. Aerosp. Sci.,2003

5. Unsteady aerodynamics of nonslender delta wings;Gursul;Prog. Aerosp. Sci.,2005

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