Investigation of Vortex Structure Behavior Induced by Different Drag Reduction Devices in the Near Field-Reference-Cited by-同舟云学术

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Investigation of Vortex Structure Behavior Induced by Different Drag Reduction Devices in the Near Field

Published:2022 Issue: Volume:65 Page:318-328
ISSN:2352-1465
Container-title:Transportation Research Procedia
language:en
Short-container-title:Transportation Research Procedia

Author:

Hrúz Michal,Pecho Pavol,Bugaj Martin,Rostáš Ján

Publisher

Elsevier BV

Subject

General Medicine

Reference24 articles.

1. Wingtip Vortices of a Biomimetic Micro Air Vehicle;Bardera;Journal of Aircraft,2022

2. Aerodynamic Analysis of Variable Cant Angle Winglets for Improved Aircraft Performance;Beechook,2013

3. Structure and Induced Drag of a Tip Vortex;Birch;Journal of Aircraft,2004

4. Analysis on Reducing the Induced Drag Using the Winglet at the Wingtip;Bojja;International Journal of Engineering Research & Technology (IJERT),2013

5. Wake vortex characteristics of transport aircraft;Breitsamter;Progress in Aerospace Sciences,2011

Cited by 1 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. INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF SWEPT C-WING CONFIGURATIONS AT TRANSONIC SPEED USING DESIGN OF EXPERIMENTS AND COMPUTATIONAL FLUID DYNAMICS;Aviation;2024-06-27

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