DEFINITION OF AIRPLANE FUSELAGE LONGITUDINAL LINES BY THE SPECIAL CONTOUR METHOD

To optimize the combined program of "fuselage-nacelle" -type surface design it is proposed to calculate all the transverse and longitudinal airplane fuselage lines by a special contour method. A block diagram is given for computer calculation of the longitudinal lines as a part of the block diagram for the design of a composite surface satisfying the optimality criteria specified in advance.

  • Corporate Authors:

    Allerton Press, Incorporated

    150 Fifth Avenue
    New York, NY  United States  10011
  • Authors:
    • Leiyushenko, S I
    • Chistyakov, F K
  • Publication Date: 1977

Media Info

  • Features: References;
  • Pagination: p. 71-73
  • Serial:

Subject/Index Terms

Filing Info

  • Accession Number: 00189729
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Files: TRIS
  • Created Date: Apr 12 1979 12:00AM