Free vibration analysis of rotating blades with uniform tapers

AIAA Journal

Volumn 42, Issue 12, 2004, Pages 2429-2437

  Wang, Gang ^a,b   Wereley, Norman M ^a,b  

^a UNIVERSITY OF MARYLAND   (United States)

^b UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); BENDING MOMENTS; FINITE ELEMENT METHOD; HELICOPTERS; MATHEMATICAL MODELS; PARTIAL DIFFERENTIAL EQUATIONS; VIBRATIONS (MECHANICAL);

BEAM TRANSVERSE DISPLACEMENTS; CENTRIFUGAL STIFFENING; ROTATING BLADES; VIBRATION ANALYSIS;

TURBOMACHINE BLADES;

EID: 10944268229     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.4302     Document Type: Article

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