Effect of a wing on its tip vortex.-Reference-Cited by-同舟云学术

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Effect of a wing on its tip vortex.

Published:1969-01 Issue:1 Volume:6 Page:37-41
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

GROW TERENCE L.¹

Affiliation:

1. The Pennsylvania State University, University Park, Pa.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.43998

Reference17 articles.

1. Tangier, J. L. "A Study of the Vortex Sheet Immediately Behind an Aircraft Wing," M.S. thesis,March 1966, The Pennsylvania Slate Univ.

2. Logan, A. H. "A Solution to the Vortex Breakdown Phenomenon in a Trailing Line Vortex," M.S. thesis,Dec. 1966, The Pennsylvania State Univ.

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2. Simulation of Wingtip Vortex Flows with Reynolds-Averaged Navier–Stokes and Scale-Resolving Simulation Methods;AIAA Journal;2019-03

3. Flow structure of a low aspect ratio wall-mounted airfoil operating in a low Reynolds number flow;Experimental Thermal and Fluid Science;2018-12

4. Tip Vortex Formation and Cavitation;Journal of Fluids Engineering;1997-06-01

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