The Design and Operation of a Simple Low-Speed Flutter-Suppression Model.

Abstract

This Australian report discusses a dynamic model which has been developed for use in a small low-speed wind tunnel. A feedback system has been used to drive a control surface in order to suppress flutter. Details of the model and results of preliminary tests are presented. Keywords include: Wind tunnel models, and Active Control.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1984
Accession Number
ADA151610

Entities

People

  • A. Goldman

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accelerometers
  • Actuators
  • Closed Loop Systems
  • Control Surfaces
  • Control Systems
  • Department Of Defense
  • Digital Computers
  • Engineering
  • Feedback
  • Frequency
  • Laboratory Equipment
  • Mathematical Analysis
  • Measurement
  • Mechanical Engineering
  • Power Amplifiers
  • Test Facilities
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Robotics and Automation.