THE DEVELOPMENT OF 3 DOF WING SECTION MODEL FOR AEROELASTIC AND ACTIVE CONTROL WIND TUNNEL EXPERIMENTAL TESTS
Congress; 27th, International Council of the Aeronautical Sciences (Congress); ICAS 2010; [electronic resource] ; 2010 ; Nice, France
International Council of the Aeronautical Sciences (Congress); ICAS 2010; [electronic resource] ; ICAS 2010-9.8.3
2010-01-01
ICAS 2010-9.8.3
Includes bibliographical references and author index; Held on CD-ROM
Conference paper
English
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