Shape Sensing of Plate and Shell Structures Undergoing Large Displacements Using the Inverse Finite Element Method

被引:52
作者
Tessler, Alexander [1 ]
Roy, Rinto [2 ]
Esposito, Marco [3 ]
Surace, Cecilia [2 ]
Gherlone, Marco [3 ]
机构
[1] NASA, Langley Res Ctr, Struct Mech & Concepts Branch, Hampton, VA 23665 USA
[2] Politecn Torino, Dept Struct Geotech & Bldg Engn, Turin, Italy
[3] Politecn Torino, Dept Mech & Aerosp Engn, Turin, Italy
关键词
Strain - Plates (structural components) - Inverse problems;
D O I
10.1155/2018/8076085
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
The inverse Finite Element Method (iFEM) is applied to reconstruct the displacement field of a shell structure which undergoes large deformations using discreet strain measurements as the prescribed data. The iFEM computations are carried out using an incremental procedure where at each load step, the incremental strains are used to evaluate the incremental displacements which in turn update the geometry of the deformed structure. The efficacy of the proposed approach to predict large displacements is examined using two case studies involving a cantilevered wing-shaped plate and a clamped plate. The incremental iFEM procedure is demonstrated to be sufficiently accurate in terms of reproducing the correct nonlinear character of the load-displacement curve even when a reduced number of strain sensors is used. Therefore, this approach may have important implications for real-time monitoring of aerospace structures that undergo large displacements.
引用
收藏
页数:8
相关论文
共 15 条
[1]   Wireless and distributed sensing of the shape of morphing structures [J].
Akl, W. ;
Poh, S. ;
Baz, A. .
SENSORS AND ACTUATORS A-PHYSICAL, 2007, 140 (01) :94-102
[2]  
Bang HJ, 2012, IEEE IMTC P, P496
[3]  
Dassault Systemes Simulia Corp, 2013, AB AN US GUID VERS 6
[4]   Shape and vibration mode sensing using a fiber optic Bragg grating array [J].
Davis, MA ;
Kersey, AD ;
Sirkis, J ;
Friebele, EJ .
SMART MATERIALS & STRUCTURES, 1996, 5 (06) :759-765
[5]   Shape sensing methods: Review and experimental comparison on a wing-shaped plate [J].
Gherlone, Marco ;
Cerracchio, Priscilla ;
Mattone, Massimiliano .
PROGRESS IN AEROSPACE SCIENCES, 2018, 99 :14-26
[6]   Shape sensing of 3D frame structures using an inverse Finite Element Method [J].
Gherlone, Marco ;
Cerracchio, Priscilla ;
Mattone, Massimiliano ;
Di Sciuva, Marco ;
Tessler, Alexander .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2012, 49 (22) :3100-3112
[7]  
Jones R. T., 1988, SMART MATER STRUCT, V7, P178
[8]   Estimation of dynamic structural displacements using fiber Bragg grating strain sensors [J].
Kang, Lae-Hyong ;
Kim, Dae-Kwan ;
Han, Jae-Hung .
JOURNAL OF SOUND AND VIBRATION, 2007, 305 (03) :534-542
[9]  
Ko W. L., 2009, NASATP200921465
[10]  
Mao Z., 2008, P SPIE