Complexity of the phenomena of panel flutter instability has resulted in the necessity of developing separate design criteria for a variety of flow conditions and panel configurations. Vehicle panel configurations with low aspect ratios are of interest in low supersonic flow, where boundary layer effects are important.
Aerodynamic forces of fluttering cylindrical and/or planar structures
1969-12-01
Miscellaneous
No indication
English
Online Contents | 1993
|Finite-element analysis of the fluttering panels excited by external forces
Online Contents | 1999
|Fatigue life estimation of fluttering panels
NTRS | 1970
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