Sample calculations presented for series of wings subject to bending vs torsion flutter, showing how natural mode dampings and frequencies change as flutter speed is approached; comparison between normal mode characteristics and system response due to forced excitation.
Study of bending-torsion aeroelastic modes for aircraft wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 16 , n 7
1949
8 pages
Diagrams
Article (Journal)
English
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Aeroelastic Response and Flutter of Swept Aircraft Wings
AIAA | 2002
|Aeroelastic response and flutter of swept aircraft wings
Tema Archive | 2002
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