Chien-Chang Lin
- Optimum design of composite wing structures by a refined optimality criterion. In: Composite Structures, v. 17, n. 1 ( 1991). (1991):
- Prediction for delamination initiation around holes in symmetric laminates. In: Composite Structures, v. 22, n. 4 ( 1992). (1992):
- Stresses in rotating composite cylindrical shells. In: Composite Structures, v. 25, n. 1-4 ( 1993). (1993):
- Stress and strength analysis of composite joints using direct boundary element method. In: Composite Structures, v. 25, n. 1-4 ( 1993). (1993):
- Adhesive interface element for bonding of laminated plates. In: Composite Structures, v. 25, n. 1-4 ( 1993). (1993):
- Engineering analysis of buckling of delaminated beam plates. In: Composite Structures, v. 34, n. 4 ( 1996). (1996):
- A conforming quadrilateral plate bending element with shear deformations. In: Computers & Structures, v. 56, n. 1 (Juli 1995). (1995):
- Vibration control of beam–plates with bonded piezoelectric sensors and actuators. In: Computers & Structures, v. 73, n. 1-5 (Oktober 1999). (1999):
- Free vibration of bonded plates. In: Computers & Structures, v. 64, n. 1-4 (Juli 1997). (1997):
- Application of array management system for the development of structural analysis programs. In: Computers & Structures, v. 41, n. 5 (Januar 1991). (1991):
- Vibration and sound radiation controls of beams using layered modal sensors and actuators. In: Smart Materials and Structures, v. 7, n. 4 (August 1998). (1998):
- Static shape control of smart beam plates laminated with sine sensors and actuators. In: Smart Materials and Structures, v. 8, n. 5 (Oktober 1999). (1999):