ANALYSIS OF PREDICTED AIRCRAFT WAKE VORTEX TRANSPORT AND COMPARISON WITH EXPERIMENT. VOLUME II. APPENDIXES

;Contents: Summary of aircraft flybys; Probable stability conditions prevalent during selected NAFEC flybys at Atlantic City, N.J.; Description of output plots of wake vortex transport computer program; Description of input requirements for Lockheed wake vortex tramsport computer program; Summary of line printer output of Lockheed wake vortex transport computer program; Flow charts for Lockheed wake vortex transport computer program; Summary of predicted wake vortex tracks and comparison with experiment; Report of inventions.

  • Supplemental Notes:
    • See also Volume 1, AD-783 649.
  • Corporate Authors:

    Lockheed Missiles and Space Company

    Huntsville Research and Engineering Center
    Huntsville, AL  USA  35807

    Transportation Systems Center

    55 Broadway, Kendall Square
    Cambridge, MA  USA  02142

    Federal Aviation Administration

    Systems R&D Service, 800 Independence Avenue, SW
    ,   USA 
  • Authors:
    • Brashears, M R
    • Logan, N A
    • Robertson, S J
    • Shrider, K R
    • Walters, C D
  • Publication Date: 1974-4

Media Info

  • Pagination: 231 p.

Filing Info

  • Accession Number: 00071881
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: Final Rpt.
  • Contract Numbers: DOT-TSC-593
  • Files: NTIS, USDOT
  • Created Date: Dec 19 1974 12:00AM