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  United States  43212

  Federal Aviation Administration

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

Media Info

• Pagination: 66 p.

Subject/Index Terms

• TRT Terms: Airborne navigational aids; Aircraft; Angle of attack; Aviation safety; Human machine systems; Information display systems; Stall
• Old TRIS Terms: Flight instruments
• Subject Areas: Aviation; Safety and Human Factors; Vehicles and Equipment;

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