Modified, discrete-vortex method for studying wing-loading effects on wake dynamics
Author:
Affiliation:
1. Rose-Hulman Institute of Technology, Terre Haute, Indiana 47803
2. University of Notre Dame, Notre Dame, Indiana 46556-5637
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46916
Reference31 articles.
1. Research on aircraft/vortex-wake interactions to determine acceptable level of wake intensity
2. Dynamic Behavior of an Aircraft Encountering Aircraft Wake Turbulence
3. An analysis of relative wake-vortex hazards for typical transport aircraft
4. Aircraft Wake Turbulence and Its Detection
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