STOCHASTIC THERMAL BUCKLING ANALYSIS OF VARIABLE ANGLE TOW COMPOSITES
被引:0
|
作者:
Thapa, Mishal
论文数: 0引用数: 0
h-index: 0
机构:
Univ Alabama, Dept Aerosp Engn & Mech, Tuscaloosa, AL 35487 USAUniv Alabama, Dept Aerosp Engn & Mech, Tuscaloosa, AL 35487 USA
Thapa, Mishal
[1
]
Zhao, Wei
论文数: 0引用数: 0
h-index: 0
机构:
Oklahoma State Univ, Sch Mech & Aerosp Engn, Stillwater, OK 74078 USAUniv Alabama, Dept Aerosp Engn & Mech, Tuscaloosa, AL 35487 USA
Zhao, Wei
[2
]
Mulani, Sameer B.
论文数: 0引用数: 0
h-index: 0
机构:
Univ Alabama, Dept Aerosp Engn & Mech, Tuscaloosa, AL 35487 USAUniv Alabama, Dept Aerosp Engn & Mech, Tuscaloosa, AL 35487 USA
Mulani, Sameer B.
[1
]
机构:
[1] Univ Alabama, Dept Aerosp Engn & Mech, Tuscaloosa, AL 35487 USA
[2] Oklahoma State Univ, Sch Mech & Aerosp Engn, Stillwater, OK 74078 USA
来源:
PROCEEDINGS OF ASME 2024 AEROSPACE STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE, SSDM2024
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2024年
关键词:
Variable angle tow laminates;
Uncertainty quantification;
Thermal buckling analysis;
Polynomial chaos expansion;
Global sensitivity Analysis;
POLYNOMIAL CHAOS;
PLATES;
UNCERTAINTY;
D O I:
暂无
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
Variable angle tow (VAT) enables tailoring the stiffness distribution across the laminates for improved structural performance by combining the features of advanced automated tape laying and filament winding. However, the performance of VAT composites is affected by the presence of uncertainties in material properties, geometric properties, loads, and boundary conditions that are unwantedly introduced during the manufacturing process. This leads to composite products that may not exactly perform as expected during the operation, which necessitates accounting for the effects of the uncertainties during the design and analysis of VAT composites. Therefore, a sparse polynomial chaos expansion (PCE)-based approach for uncertainty quantification (UQ) and global sensitivity analysis of the thermal buckling response of a variable angle tow (VAT) laminate is presented. Two test cases are considered for thermal buckling analysis of a VAT laminate under material and geometric uncertainties- similar random properties for different plies and different random properties for different plies. Furthermore, the effect of assumption regarding the distribution of random parameters is also studied by considering normal and uniform distribution. The results have been verified with a large number of Monte Carlo Simulations. The results underlined the benefits of using a PCE-based approach for quantifying the effects of uncertainties on the thermal buckling response of VAT laminate and identifying the influential random parameters.