A Flight Dynamic Model of Aircraft Spinning

Abstract

A flight dynamic model of aircraft spinning been developed. It is capable of simulating aircraft behaviour from conventional flight through stall, spin entry, steady spin, and spin recovery. A data base storage technique has been used to provide the six force and moment coefficients required. The data base embodies rotary balance data measured for a basic training aircraft plus computed small disturbance data calculated from a line vortex model. Keywords: Training aircraft; Spinning motion; Trim aerodynamics; Angular motion; Mathematical predication; Computerized simulation; Vortices/oscillation; Australia.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1990
Accession Number
ADA228450

Entities

People

  • C. A. Martin
  • S. D. Hill

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aerodynamics
  • Aircrafts
  • Angular Motion
  • Australia
  • Basic Training
  • Databases
  • Flight
  • Fluid Mechanics
  • Mechanical Engineering
  • Mechanics
  • Simulations
  • Spin Recovery
  • Three Dimensional
  • Time Intervals
  • Training
  • Training Aircraft

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aviation Science / Aeronautics.
  • Computer Science.