Formulation of an aircraft structural uncertainty model for robust flutter predictions

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 5, Issue , 2004, Pages 3648-3662

  Danowsky, Brian P ^a,c   Chavez, Frank R ^a,c   Brenner, Marty ^b,d  

^a IOWA STATE UNIVERSITY   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^c 2271 Howe Hall ^*  (United States)

^d NASA DFRC

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC FORCES; DYNAMIC INSTABILITY; PARAMETRIC UNCERTAINTY; PRESSURE COEFFICIENT VECTORS;

AIRCRAFT; EQUATIONS OF MOTION; FLIGHT DYNAMICS; MATHEMATICAL MODELS; MODAL ANALYSIS; NATURAL FREQUENCIES; OSCILLATIONS; ROBUSTNESS (CONTROL SYSTEMS); STIFFNESS; STRUCTURAL DESIGN; UNCERTAIN SYSTEMS; VECTORS; WINGS;

FLUTTER (AERODYNAMICS);

EID: 16244376758     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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