An experimental study on the effect of a novel nature-inspired 3D-serrated leading edge on the aerodynamic performance of a double delta wing in the transitional flow regime-Reference-Cited by-同舟云学术

An experimental study on the effect of a novel nature-inspired 3D-serrated leading edge on the aerodynamic performance of a double delta wing in the transitional flow regime

Published:2019-12 Issue:12 Volume:33 Page:5913-5921
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Naeini Hamed Khodabakhshian,Nili-Ahmadabadi Mahdi,Kim Kyung Chun

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-019-1136-x.pdf

Reference30 articles.

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2. N. Verhaagen et al., A study of the vortex flow over a 76/40-deg double-delta wing, 33rd Aerosp. Sci. Meet. Exhib. (1995) 650.

3. R. Lynn and I. Gursul, Vortex dynamics on a generic UCAV configuration, 44th AIAA Aerosp. Sci. Meet. Exhib. (2006) 61.

4. Q. Deng et al., Effect of oscillating leading-edge flaps on vortices over a delta wing, 4th Shear Flow Control Conf. (1997) 1972.

5. G. Taylor et al., Lift enhancement over flexible nonslender delta wings, AIAA J., 45 (12) (2007) 2979–2993.

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