Investigation of Helicopter Rotor-Blade-Tip-Vortex Alleviation Using a Slotted Tip
Author:
Affiliation:
1. Yeungnam University, Gyongsan 712-749, Republic of Korea
2. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.3254
Reference34 articles.
1. Challenges in Understanding the Vortex Dynamics of Helicopter Rotor Wakes
2. Helicopter rotor tip shapes for reduced blade vortex interaction - An experimental investigation
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