Visualization and PIV study of wing-tip vortices for three different tip configurations-Reference-Cited by-同舟云学术

Visualization and PIV study of wing-tip vortices for three different tip configurations

Published:2012-01 Issue:1 Volume:16 Page:40-46
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sohn Myong Hwan,Chang Jo Won

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

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2. An active-control system for breakup of airplane trailing vortices;Crouch;AIAA J.,2001

3. K. Duraisamy, J.D. Baeder, Numerical simulation of the effects of spanwise blowing on wing-tip vortex formation and evolution, AIAA 2005-4726, 2005.

4. S.G. Flechner, P.F. Jacobs, R.T. Whitcomb, A high subsonic speed wind-tunnel investigation of winglets on a representative second-generation jet transport wing, NASA TN D-8264, 1976.

5. Effects of winglet dihedral on a tip vortex;Gerontakos;J. Aircraft,2006

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