REDUCED UNCERTAINTIES IN THE ROBUST FLUTTER ANALYSIS OF THE AEROSTRUCTURES TEST WING
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 2010-9.6.1
2010-01-01
ICAS 2010-9.6.1
Includes bibliographical references and author index; Held on CD-ROM
Conference paper
English
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Flutter Analysis of Aerostructures Test Wing with Test Validated Structural Dynamic Model
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