SUPERELEMENT METHOD FOR HELICOPTER FUSELAGE ANALYSIS

A solution is presented of the problem of helicopter fuselage analysis based on the finite element method in the force method variant by dividing the fuselage into segments and subsequently joining the segments with the same accuracy which is achieved in the calculation using the undivided scheme. An explanation of the algorithmization of the theory is given and results are presented from application of the method to analysis of actual fuselages.

  • Corporate Authors:

    Allerton Press, Incorporated

    150 Fifth Avenue
    New York, NY  United States  10011
  • Authors:
    • Aksenov, O M
    • Burman, Z I
  • Publication Date: 1977

Media Info

  • Features: References;
  • Pagination: p. 7-11
  • Serial:

Subject/Index Terms

Filing Info

  • Accession Number: 00189727
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Files: TRIS
  • Created Date: Apr 12 1979 12:00AM