DEVELOPMENT OF STALL DETERRENT DEVICE FOR SMALL AIRPLANES

A kinesthetic-tactual display may be effectively used as a control aid, per previous flight tests. Angle-of-attack (AOA) information would be continuously presented to a pilot, via this display, during critical operational phases -- approaches to landing, takeoff and departures, and accelerated maneuvers -- where stalls are probable. He would then have a continuous indication of aerodynamic state, and thus perform the necessary control before a stall condition was reached

  • Corporate Authors:

    Ohio State University, Columbus

    Research Foundation, 1314 Kinnear Road
    Columbus, OH  USA  43212

    Federal Aviation Administration

    800 Independence Avenue, SW
    Washington, DC  USA  20591
  • Authors:
    • Gilson, R D
    • Fenton, R W
  • Publication Date: 1975-6

Media Info

  • Pagination: 66 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00092020
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: DSURF-3962-FR Final Rpt., FAA-RD-75-53
  • Contract Numbers: DOT-FA74WA-3515
  • Files: NTIS, USDOT
  • Created Date: Oct 18 1976 12:00AM