Extension of the g-method flutter solution to aeroservoelastic stability analysis

Journal of Aircraft

Volumn 42, Issue 3, 2005, Pages 789-792

  Karpel, M ^a,c   Moulin, B ^a,d   Chen, P C ^b  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b ZONA TECHNOLOGY INC   (United States)

^c Department of Aerospace Engineering ^*  (Israel)

^d Faculty of Aerospace Engineering

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; APPROXIMATION THEORY; BOUNDARY CONDITIONS; CONTROL SYSTEM ANALYSIS; DAMPING; INTERPOLATION; MATHEMATICAL MODELS; STRUCTURAL DESIGN; VELOCITY MEASUREMENT;

AERODYNAMIC APPROXIMATION; G-METHOD FORMULATION; HARMONIC MOTION; VELOCITY-DENSITY PAIRS;

FLUTTER (AERODYNAMICS);

EID: 22544457510     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.10686     Document Type: Article

References (11)

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