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

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

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

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b ZONA TECHNOLOGY INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SURFACES; CONTROL SYSTEM STABILITY; EIGENVALUES AND EIGENFUNCTIONS; EQUATIONS OF MOTION; EQUATIONS OF STATE; FLIGHT CONTROL SYSTEMS; FLUTTER (AERODYNAMICS); FREQUENCY DOMAIN ANALYSIS; ITERATIVE METHODS; STATE SPACE METHODS; STRUCTURAL DYNAMICS;

AERODYNAMIC COEFFICIENTS; AEROSERVOELASTIC STABILITY; FIRST-ORDER APPROXIMATIONS; ITERATIVE EIGENVALUE PROBLEM; NUMERICAL APPLICATIONS; PREDICTOR CORRECTOR; SOLUTION TECHNIQUES; STATE - SPACE MODELS;

AEROSERVOELASTICITY;

EID: 85085773008     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1512     Document Type: Conference Paper

References (11)

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