Structural Assessment of Advanced Tow-Steered Shells
Author:
Affiliation:
1. NASA Langley Research Center
2. University of Bath
Publisher
American Institute of Aeronautics and Astronautics
Reference13 articles.
1. Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response
2. A. Blom, M. Rassaian, P. B. Stickler and Z. Gürdal: ModalTestingofaCompositeCylinder with Circumferentially Varying Stiffness. Proceedings of the 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. PalmSprings,California,May4-7,2009. Paperno.AIAA 2009-2558.
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1. Experimental and numerical studies on buckling and post-buckling behavior of T-stiffened variable stiffness panels;Chinese Journal of Aeronautics;2024-08
2. Manufacture and Buckling Test of a Variable-Stiffness, Variable-Thickness Composite Cylinder Under Axial Compression;AIAA Journal;2023-04
3. Nonlinear Buckling and Postbuckling Analysis of Tow-Steered Composite Cylinders with Cutouts;AIAA Journal;2022-09
4. Nonlinear Buckling Analysis of Tow-Steered Composite Cylinders with Cutouts;AIAA SCITECH 2022 Forum;2022-01-03
5. Manufacture and buckling test of a variable-stiffness, variable-thickness composite cylinder under axial compression;AIAA SCITECH 2022 Forum;2022-01-03
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