MOVING LOAD ON A LAMINATED COMPOSITE

A solution is presented for the dynamic response of a periodically laminated half plane that consists of alternating layers of two different materials and is subjected to a moving load. The laminations are parallel to the surface of the half plane, and the velocity of the load is steady and supersonic. An effective stiffness theory developed by Sun, Achenbach, and Herrmann is used to model the layered material, and the formal solution is obtained with the aid of Laplace transforms. A far-field solution is constructed with the head-of-the-pulse procedure, and several numerical examples are presented.

  • Corporate Authors:

    American Society of Mechanical Engineers

    Two Park Avenue
    New York, NY  United States  10016-5990
  • Authors:
    • Sve, C
    • HERRMANN, G
  • Publication Date: 1974-9

Media Info

  • Features: Appendices; Figures;
  • Pagination: p. 663-666
  • Serial:
    • ASME Transactions
    • Volume: 41
    • Issue Number: 3
    • Publisher: American Society of Mechanical Engineers

Subject/Index Terms

Filing Info

  • Accession Number: 00071758
  • Record Type: Publication
  • Source Agency: ASME Transactions
  • Report/Paper Numbers: Series E
  • Files: TRIS
  • Created Date: Dec 13 1974 12:00AM