Aeroelastic coupling of geometrically nonlinear structures and linear unsteady aerodynamics: Two formulations

Journal of Fluids and Structures

Volumn 25, Issue 5, 2009, Pages 918-935

  Demasi, L ^a   Livne, E ^b  

^a AGC Paul S Roel Chair in Construction Engineering and Management   (United States)

^b UNIVERSITY OF WASHINGTON   (United States)

Author keywords

Delta wing; Flutter; Joined wing; Newmark method; Newton Raphson method; Nonlinear aeroelasticity; Transient analysis; Unsteady aerodynamics

Indexed keywords

DELTA WING; FLUTTER; JOINED WING; NEWMARK METHOD; NONLINEAR AEROELASTICITY; UNSTEADY AERODYNAMICS;

AIRCRAFT PARTS AND EQUIPMENT; ASPECT RATIO; CONTROL NONLINEARITIES; DELTA WING AIRCRAFT; ELASTIC WAVES; ELASTICITY; FLUTTER (AERODYNAMICS); GAS DYNAMICS; INVERSE KINEMATICS; NEWTON-RAPHSON METHOD; TRANSIENT ANALYSIS;

WINGS;

EID: 67651208524     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2009.03.001     Document Type: Article

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