A study of thermal buckling of stiffened cylindrical shells with the proportions of a preliminary supersonic transport fuselage design (1970) is presented. The buckling analysis is performed using an axisymmetric shell-of-revolution code, BOSOR4. The effects of combined mechanical (axial loading) and thermal loading (heated skins) are investigated. Results indicate that the location of longitudinal eccentric stiffening has a very large effect on the thermal buckling strength of longitudinally stiffened shells, and on longitudinally stiffened shells with rings.
Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells
Einfluß von Versteifung und mechanischer Beanspruchung auf das thermische Beulen von versteiften Zylinderschalen
1995
9 Seiten, 13 Bilder, 5 Tabellen, 6 Quellen
Conference paper
English
Stiffening and Mechanical Load Effects on Thermal Buckling of Stiffened Cylindrical Shells
Online Contents | 2009
|Stiffening and Mechanical Load Effects on Thermal Buckling of Stiffened Cylindrical Shells
British Library Conference Proceedings | 2009
|Effects of Stiffeneing and Mechanical Load on Thermal Buckling of Stiffened Cylindrical Shells
British Library Conference Proceedings | 1995
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