Rigid Body Stability Augmentation Studies for a Wind Tunnel Flutter Model.

Abstract

The report describes a simulation study undertaken in preparation for wind tunnel trials of flutter suppression control laws at DFVLR, Goettingen, West Germany. Keywords; Digital simulation; Dynamic response; Flutter suppression; Wind tunnel stability tests; Stability; Feedback control; Tornado aircraft; Computer aircraft; Computer programs; Australia.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1985
Accession Number
ADA165847

Entities

People

  • C. J. Ludowyk

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Actuators
  • Air Force
  • Aircrafts
  • Australia
  • Computer Programs
  • Control Surfaces
  • Control Systems
  • Department Of Defense
  • Dynamic Pressure
  • Dynamic Response
  • Equations Of Motion
  • Feedback
  • Resonant Frequency
  • Simulations
  • Trim Angle
  • Wind
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Atmospheric Science/Meteorology
  • Control Systems Engineering.