Buckling Analysis of Triangularly Stiffened Cylindrical Panels and their Application to Aircraft Structures-Reference-Cited by-同舟云学术

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Buckling Analysis of Triangularly Stiffened Cylindrical Panels and their Application to Aircraft Structures

Published:2008-04-07 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t
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Author:

Klinzmann Astrid,Horst Peter

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. 1Burchard, W., Beulspannungen der quadratischen Platte mit Schragsteife unter Druck bzw. Schub, Ingenieurarchiv, Vol.21, 1937.

2. 3Heitmann, M., Untersuchung des Nachbeulverhaltens rechteckig versteifter metallischer Strukturen unter kombinierter Druck- und Schubbeanspruchung, Dissertation TU Braunschweig, 2005.

3. 5Kébreau, S., Fracture mechanics analysis of novel non-rectangular stiffening concepts in comparison to conventionally rectangular stiffened fuselage structures, Proceedings of the first CEAS congress, 2007.

4. 6Kiehne, A., Horst, P., Buckling analysis of non-rectangular stiffened shell structures, Jahrbuch der DGLR-Jahrestagung, 2006.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Non-prismatic sub-stiffening for stiffened panel plates—Stability behaviour and performance gains;Thin-Walled Structures;2010-06

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