Real-Time Characterization of Aerospace Structures Using Onboard Strain Measurement Technologies and Inverse Finite Element Method

被引:0
作者
Tessler, A. [1 ]
Spangler, J. L. [2 ]
Mattone, M. [3 ]
Gherlone, M. [3 ]
Di Sciuva, M.
机构
[1] NASA, Langley Res Ctr, Struct Mech & Concepts Branch, Mail Stop 190, Hampton, VA 23681 USA
[2] Lockheed Martin Aeronaut Co, Hampton, VA 23681 USA
[3] Politecn Torino, Dept Aeronaut & Space Engn, I-10129 Turin, Italy
来源
STRUCTURAL HEALTH MONITORING 2011: CONDITION-BASED MAINTENANCE AND INTELLIGENT STRUCTURES, VOL 1 | 2011年
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中图分类号
R5 [内科学];
学科分类号
1002 ; 100201 ;
摘要
The inverse problem of real-time reconstruction of full-field structural displacements, strains, and stresses is addressed using an inverse finite element method based on shear deformable shell finite element technology. Utilizing surface strain measurements from strain sensors mounted on load-carrying structural components, the methodology enables accurate computations of the three-dimensional displacement field for a general built-up shell structure undergoing multi-axial deformations. The strain and stress computations are then carried out at the element level using strain-displacement and constitutive relations. This high fidelity computational technology is essential for providing feedback to the actuation and control systems of the next generation of aerospace vehicles, and for assessing real-time internal loads and structural integrity.
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页码:981 / +
页数:2
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