Supersonic flutter of laminated circular cylindrical shell panels

The present flutter analysis gives attention to circular cylindrical shell panels of rectangular planform whose edges are clamped laterally and free from in-plane stresses. The panel is acted upon by supersonic flow parallel to the generator on one of its sides. The aerodynamic forces are approximat...

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Veröffentlicht in:	Journal of aircraft 1991-08, Vol.28 (8), p.543-544
Hauptverfasser:	Srinivasan, R. S, Babu, B. J. C
Format:	Artikel
Sprache:	eng
Schlagworte:	Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Structural and continuum mechanics Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
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Beschreibung
Zusammenfassung:	The present flutter analysis gives attention to circular cylindrical shell panels of rectangular planform whose edges are clamped laterally and free from in-plane stresses. The panel is acted upon by supersonic flow parallel to the generator on one of its sides. The aerodynamic forces are approximated by means of two-dimensional quasi-steady aerodynamic theory, and the solution is obtained by means of the integral equation technique. (O.C.)
ISSN:	0021-8669 1533-3868
DOI:	10.2514/3.46061