New consideration on flutter properties based on step-by-step analysis

Journal of Wind Engineering and Industrial Aerodynamics

Volumn 98, Issue 8-9, 2010, Pages 429-437

  Matsumoto, Masaru ^a   Matsumiya, Hisato ^b   Fujiwara, Shinya ^c   Ito, Yasuaki ^d  

^a KYOTO UNIVERSITY   (Japan)

^b CENTRAL RESEARCH INSTITUTE OF ELECTRIC POWER INDUSTRY   (Japan)

^c OSAKA GAS CO LTD   (Japan)

^d SHIMIZU CORPORATION   (Japan)

Author keywords

2DOF coupling flutter affected by structural coupling; Fundamental flutter mode; Selberg's formula; Step by step analysis; Torsional divergence velocity

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); STRUCTURAL ANALYSIS;

FUNDAMENTAL FLUTTER MODE; SELBERG'S FORMULA; STEP-BY-STEP ANALYSIS; STRUCTURAL COUPLING; TORSIONAL DIVERGENCE;

FLUTTER (AERODYNAMICS);

EID: 77953360095     PISSN: 01676105     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jweia.2010.02.001     Document Type: Article

References (7)

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3. Matsumoto, M., Matsumiya, H., Fujiwara, S., Ito, Y., 2008. On flutter fundamental modes, reduction of similar Selberg's formula and torsional divergence instability basing on SBSA, 6th BBAA.
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