Wing Tip Vortex in the Near Field: An Experimental Study-Reference-Cited by-同舟云学术

Wing Tip Vortex in the Near Field: An Experimental Study

Published:2005-09 Issue:5 Volume:42 Page:1366-1368
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Lombardi Giovanni¹,Skinner Peter²

Affiliation:

1. University of Pisa, 56122 Pisa, Italy

2. Defencetek—CSIR, Pretoria 0001, South Africa

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.12314

Reference5 articles.

1. Canard tip vortex splitting in a canard-wing configuration - Experimental observations

2. Vorticity measurement by a pressure probe

3. 3Engel, M. "A Wind Tunnel Investigation of a Wing-Tip Trailing Vortex," MS thesis, AOE Dept,Virginia Polytechnic Institute and State University, Blacksburg, VA,1995.

4. The structure and development of a wing-tip vortex

5. Measurements in Rollup Region of the Tip Vortex from a Rectangular Wing

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