State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading

Journal of Aircraft

Volumn 33, Issue 4, 1996, Pages 816-822

  Frampton, Kenneth D ^a,b   Clark, Robert L ^a,b   Dowell, Earl H ^a,c  

^a DUKE UNIVERSITY   (United States)

^b Dept of Mech Eng and Mat Science ^*

^c Aerospace Engineering Group

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; APPROXIMATION THEORY; BOUNDARY CONDITIONS; DIGITAL FILTERS; FEEDBACK; FLUTTER (AERODYNAMICS); FUNCTIONS; MATHEMATICAL MODELS; NUMERICAL METHODS; POTENTIAL FLOW; STATE SPACE METHODS; STRUCTURAL PANELS;

AERODYNAMIC FORCE; AERODYNAMIC FUNCTIONS; AEROELASTIC PANELS; PANEL FLUTTER BOUNDARIES; PRONYS METHOD; STATE SPACE MODELING;

AEROSPACE ENGINEERING;

EID: 0030193495     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47019     Document Type: Article

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