Influence of Differential Spoiler Settings on the Wake Vortex Characterization and Alleviation
Author:
Affiliation:
1. International Islamic University Malaysia, Gombak, Kuala Lumpur 53100
2. Korea Aerospace Research Institute, Deajeon 305-333, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C000258
Reference13 articles.
1. Airplane trailing vortices and their control
2. Vortex Interactions in Multiple Vortex Wakes behind Aircraft
3. Experimental Study of the Effect of Span Loading on Aircraft Wakes
4. "Minimised Wake": a Collaborative Research Programme on Aircraft Wake Vortices
5. Method for Accelerating the Destruction of Aircraft Wake Vortices
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