Dynamic Load Alleviation in Wake Vortex Encounters
Author:
Affiliation:
1. ETH Zurich, 8092 Zurich, Switzerland
2. Imperial College, London, England SW7 2AZ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G000715
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1. An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft
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