The usability of the general aviation synthesis program (GASP) was enhanced by the development of separate computer subroutines which can be added as a package to this assembly of computerized design methods or used as a separate subroutine program to compute the dynamic longitudinal, lateral-directional stability characteristics for a given airplane. Currently available analysis methods were evaluated to ascertain those most appropriate for the design functions which the GASP computerized design program performs. Methods for providing proper constraint and/or analysis functions for GASP were developed as well as the appropriate subroutines.

  • Corporate Authors:

    Center for Research, Incorporated

    Kansas University, 2385 Irving Road
    Lawrence, KS  United States  66045
  • Authors:
    • Keppel, B V
    • Eysink, H
    • Hammer, J
    • Hawley, K
    • Meredith, P
  • Publication Date: 1978-5-12

Media Info

  • Pagination: 457 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00181685
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: NASA-CR-157210 Stat Rpt.
  • Contract Numbers: NSG-2145
  • Files: TRIS
  • Created Date: Oct 31 1979 12:00AM