Accession Number:

ADA012387

Title:

Development of Stall Deterrent Device for Small Airplanes.

Descriptive Note:

Final rept. 26 Jun 74-25 Jan 75,

Corporate Author:

OHIO STATE UNIV RESEARCH FOUNDATION COLUMBUS

Personal Author(s):

Report Date:

1975-06-01

Pagination or Media Count:

66.0

Abstract:

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

Subject Categories:

  • Aircraft
  • Flight Control and Instrumentation

Distribution Statement:

APPROVED FOR PUBLIC RELEASE