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  United States  35807

  Transportation Systems Center

  55 Broadway, Kendall Square
  Cambridge, MA  United States  02142

  Federal Aviation Administration

  Systems R&D Service, 800 Independence Avenue, SW
  Washington, DC  United States 
• 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