Modeling Wake Vortex Roll-Up and Vortex-Induced Forces and Moments for Tight Formation Flight
Author:
Affiliation:
1. Technical University of Berlin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5076
Reference16 articles.
1. F/A-18 Aircraft Performance Benefits Measured During the Autonomous Formation Flight Project
2. An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft
3. Modeling and Simulation of Wake Vortex Encounters: State-of-the-Art and Challenges
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