Impact identification of stiffened composite panels: I. System development

被引:151
作者
Seydel, R [1 ]
Chang, FK [1 ]
机构
[1] Stanford Univ, Stanford, CA 94305 USA
关键词
D O I
10.1088/0964-1726/10/2/323
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
An investigation was conducted to develop a real-time identification technique for the prediction of the location and force history of low-velocity impacts on composite panels with beam stiffeners. The investigation included both analysis and experiments. Measurements from built-in piezoceramic sensors were used to reconstruct the force history using the smoother-filter algorithm. Impact location was determined by minimizing the difference between modeled response and actual response. Computer codes were developed for model construction (WFMODEL) and impact identification (WIDIMPACT). The model allowed for the variation of plate structural properties (density and stiffness) due to the presence of stiffeners. Results of extensive experiments verified the model, as coded in WFMODEL, for impacts both in the bay and on the stiffener. The identification technique, as implemented in the code WIDIMPACT, demonstrated real-time capability. Good agreement was found between predicted and actual force history and location, with success for different impact masses.
引用
收藏
页码:354 / 369
页数:16
相关论文
共 31 条
[1]   Recovery of impact contact forces of composite plates using fiber optic sensors and neural networks [J].
Akhavan, F ;
Watkins, SE ;
Chandrashekhara, K .
FIBER OPTIC AND LASER SENSORS XIV, 1996, 2839 :277-288
[2]   Estimation of contact force on composite plates using impact induced strain and neural network [J].
Chandrashekhara, K ;
Okafor, AC ;
Jiang, YP .
SMART STRUCTURES AND MATERIALS 1996: SMART SENSING, PROCESSING, AND INSTRUMENTATION, 1996, 2718 :320-330
[3]  
CHEN HJ, 1996, THESIS STANFORD U
[4]   Identification of impact force and location using distributed sensors [J].
Choi, KY ;
Chang, FK .
AIAA JOURNAL, 1996, 34 (01) :136-142
[5]  
Doyle J.F., 1997, WAVE PROPAGATION STR
[7]   SIMPLE EXPRESSIONS FOR HIGHER VIBRATION MODES OF UNIFORM EULER BEAMS [J].
DUGUNDJI, J .
AIAA JOURNAL, 1988, 26 (08) :1013-1014
[8]   EQUIVALENT PLATE ANALYSIS OF AIRCRAFT WING BOX STRUCTURES WITH GENERAL PLANFORM GEOMETRY [J].
GILES, GL .
JOURNAL OF AIRCRAFT, 1986, 23 (11) :859-864
[9]  
GUNTHER MF, 1993, P SOC PHOTO-OPT INS, V1798, P262, DOI 10.1117/12.141322
[10]   PARAMETER-IDENTIFICATION OF LINEAR-SYSTEMS BASED ON SMOOTHING [J].
IDAN, M ;
BRYSON, AE .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (04) :901-911