Near Ground Aircraft Wake Dissipation with Obstacles
Author:
Affiliation:
1. Nanyang Technological University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3298
Reference13 articles.
1. Enhancement of aircraft wake vortex decay in ground proximity
2. Aircraft Wake-Vortex Decay in Ground Proximity—Physical Mechanisms and Artificial Enhancement
3. Wake Vortex Evolution During Approach and Landing With and Without Plate Lines
4. Laser-Doppler system for detection of aircraft trailing vortices
5. 5Gardoz, L., Lawrence, D., and Miller, N. “The Measurements of the Boeing 747 Trailing Vortex System Using the Tower Fly-By Technique,” Tech. Rep. FAA-RD-73-156, Federal Aviation Administration, 1973.
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2. Numerical Optimization of Plate-Line Design for Enhanced Wake-Vortex Decay;Journal of Aircraft;2017-05
3. Effect of Ground Obstacle Separation Distance on Wake Vortex Dissipation;34th AIAA Applied Aerodynamics Conference;2016-06-10
4. Effect of Ground Obstacle of Different Aspect Ratio on Wake Vortex Dissipation (Invited);8th AIAA Atmospheric and Space Environments Conference;2016-06-10
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