Flutter boundary prediction based on nonstationary data measurement

Journal of Aircraft

Volumn 34, Issue 3, 1997, Pages 427-432

  Torii, Hiroshi ^a,c,d   Matsuzakit, Yuji ^b,c,d  

^a MEIJO UNIVERSITY   (Japan)

^b NAGOYA UNIVERSITY   (Japan)

^c Dept of Vehicle System Engineering ^*

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; MODAL ANALYSIS; SYSTEM STABILITY; TIME DOMAIN ANALYSIS; WIND TUNNELS;

BENDING TORSION WING MODEL; FLUTTER BOUNDARY;

WINGS;

EID: 0031146961     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2187     Document Type: Article

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