Simulation of Counter-Rotating Vortex Pairs on a Triangular-Flapped Wing with Flap-Tip Free Vortex Modeling-Reference-Cited by-同舟云学术

Simulation of Counter-Rotating Vortex Pairs on a Triangular-Flapped Wing with Flap-Tip Free Vortex Modeling

Published:2018-09-08 Issue:4 Volume:19 Page:805-815
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Kang Woo-Ram,Park Se Hwan,Lee Duck-Joo

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/article/10.1007/s42405-018-0075-6/fulltext.html

Reference15 articles.

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2. Tittsworth JA, Lang SR, Johnson EJ, Barnes S (2012) Federal aviation administration wake turbulence program-recent highlights. In: Proceedings of 57th air traffic control association annual conference & exposition, pp 1–8

3. Ortega JM, Bristol RL, Savas Ö (2003) Experimental study of the instability of unequal-strength counter-rotating vortex pairs. J Fluid Mech 474:35–84

4. Ortega JM, Bristol RL, Savas Ö (2002) Wake alleviation properties of triangular flapped wings. AIAA J 40:709–721

5. Allen A, Breitsamter C (2009) Experimental investigation of counter-rotating four vortex aircraft wake. Aerosp Sci Technol 13(2–3):114–129

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1. Research on Aircraft Wake Vortex Evolution and Wake Encounter in Upper Airspace;International Journal of Aeronautical and Space Sciences;2022-01-10

2. Correction to: Simulation of Counter-Rotating Vortex Pairs on a Triangular-Flapped Wing with Flap-Tip Free Vortex Modeling;International Journal of Aeronautical and Space Sciences;2018-10-24