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The structural performance of two advanced composite tow-steered shells, manufactured using a fiber placement system, is assessed using both experimental and analytical methods. The fiber orientation angles vary continuously around the shell circumference from ±10 degrees on the shell crown and keel, to ±45 degrees on the shell sides. The two shells differ in that one shell has the full 24-tow course applied during each pass of the fiber placement system, while the second shell uses the fiber placement system's tow drop/add capability to achieve a more uniform shell wall thickness. The shells are tested in axial compression, and estimates of their prebuckling axial stiffnesses and bifurcation buckling loads are predicted using linear finite element analyses. These preliminary predictions compare well with the test results, with an average agreement of approximately 10 percent.
|Title of host publication||54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference|
|Publisher||American Institute of Aeronautics and Astronautics|
|Publication status||Published - Apr 2013|
|Event||54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Boston, MA, USA United States|
Duration: 8 Apr 2013 → 11 Apr 2013
|Conference||54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference|
|Country/Territory||USA United States|
|Period||8/04/13 → 11/04/13|
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- 1 Finished
1/04/10 → 30/09/14
Project: Research council