High-order finite elements reduced models for use in flutter design tool

Journal of Aircraft

Volumn 42, Issue 3, 2005, Pages 748-754

  Lisandrin, Paolo ^a,b   Van Tooren, Michel ^a,b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b Faculty ot Aerospace Engineering   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DEGREES OF FREEDOM (MECHANICS); ERRORS; FINITE ELEMENT METHOD; OPTIMIZATION; STIFFNESS; STRAIN; STRUCTURAL DESIGN; TORSIONAL STRESS;

FLUTTER DESIGN; FLUTTER DESIGN TOOL; MULTIDISCIPLINARY OPTIMIZATION; NORMAL STRESSES;

FLUTTER (AERODYNAMICS);

EID: 22544486002     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.9824     Document Type: Article

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