Effects of Perpendicular Blade-Vortex Interaction, Part 1: Turbulence Structure and Development
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0203
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7527
Reference24 articles.
1. Effect of tip vortex structure on helicopter noise due to blade-vortex interaction
2. Aerodynamics of two-dimensional blade-vortex interaction
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4. Distortion of the vortex core during blade-vortex interaction
5. Main Rotor Broadband Noise Study in the DNW
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