Coupled Vortex-Lattice Flight Dynamic Model with Aeroelastic Finite-Element Model of Flexible Wing Transport Aircraft with Variable Camber Continuous Trailing Edge Flap for Drag Reduction (AIAA 2013-4746)
Conference, Atmospheric flight mechanics ; 2013 ; Boston, MA
2013-01-01
38 pages
Includes bibliographical references and index
Conference paper
English
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