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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (12): 1502-1506.

• 论文 • Previous Articles     Next Articles

SEMI-ANALYTICAL SOLUTION FOR THE FREE VIBRATION OF THICK-WALL AND LAMINATED ORTHOTROPIC STRUCTURES

Wang Zhiguo1, Zhi Demao1, Tang Limin2   

  1. Nanjing University of Aeronautics and Astronautics, Nanjing, 210016;Dalian University of Technology, Dalian, 116023
  • Received:1993-12-20 Revised:1994-03-12 Online:1994-12-25 Published:1994-12-25

Abstract: Canonical equations of elasticity and its corresponding variational principle are presented,a Hamilton element and a semi-analytical numerical method are developed,and finally two numerical examples are given,i.e.a deep beam and a laminated thick orthotropic plate.

Key words: elastodynamics, hamilton element, thickwall-laminated structure

CLC Number: