Initial Assessment of a Variable-Camber Continuous Trailing-Edge Flap System for Drag-Reduction of Non-Flexible Aircraft in Steady-State Cruise Condition (AIAA 2013-5143)
Conference, Infotech@aerospace ; 2013 ; Boston, MA
2013-01-01
22 pages
Includes bibliographical references and index
Conference paper
English
Infotech , Aeronautics , Astronautics , AIAA , Aerospace
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