Minimum Induced Drag Conditions for Winglets: the Best Winglet Design Concept-Reference-Cited by-同舟云学术

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Minimum Induced Drag Conditions for Winglets: the Best Winglet Design Concept

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
language:
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Author:

Demasi Luciano¹,Monegato Giovanni²,Cavallaro Rauno³,Rybarczyk Rachel¹

Affiliation:

1. San Diego State University

2. Technical University of Turin

3. Charles III University of Madrid

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2301

Reference43 articles.

1. DRAG DUE TO LIFT: Concepts for Prediction and Reduction

2. Experimental Investigation of Wing-Tip Devices on the Reduction of Induced Drag

3. Induced Drag - Historical Perspective

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design and Analysis of Generic UAV Composite Winglet Structures;Journal of The Institution of Engineers (India): Series C;2023-07-26

2. Aerodynamic Analysis of a Box Winglet: Viscous and Compressible Flow Predictions;Aerotecnica Missili & Spazio;2022-07-23

3. Design and analysis of variable camber wing of propeller aircraft using the actuator disc method;The Aeronautical Journal;2022-03-24

4. AN ALTERNATIVE APPROACH TO INDUCED DRAG REDUCTION;Aviation;2021-11-10

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