Effect of winglets induced tip vortex structure on the performance of subsonic wings-Reference-Cited by-同舟云学术

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Effect of winglets induced tip vortex structure on the performance of subsonic wings

Published:2016-11 Issue: Volume:58 Page:328-340
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Narayan Gautham,John Bibin^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Fundamentals of Aerodynamics;Anderson,2011

2. Why aircraft fly;Auerbach;Eur. J. Phys.,2000

3. Theory of Wing Sections, Including a Summary of Airfoil Data;Abbott,1959

4. Induced-drag minimization of nonplanar geometries based on the Euler equations;Hicken;AIAA J.,2010

5. A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets;Whitcomb,1976

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