Enhancing lift and reducing wingtip vortices using a passive rotor on finite-span wings-Reference-Cited by-同舟云学术

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Enhancing lift and reducing wingtip vortices using a passive rotor on finite-span wings

Published:2024-03 Issue: Volume:146 Page:108918
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Deb Dipan^ORCID,Elmaradny Abdelrahman A.^ORCID,Huang Kevin,Fouda Moatasem,Taha Haithem E.

Funder

Air Force Office of Scientific Research

National Science Foundation

Publisher

Elsevier BV

Reference28 articles.

1. The effect of staggering a biplane;Norton,1921

2. An experimental and theoretical analysis of the aerodynamic characteristics of a biplane-winglet configuration;Gall,1984

3. L. Prandtl, Tragflügeltheorie, 1918.

4. A. Pope, Basic wing and airfoil theory (No Title), 1951.

5. Aerodynamic characteristics of dragonfly wing sections compared with technical aerofoils;Kesel;J. Exp. Biol.,2000

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