Research and Development of Aircraft Control Actuation Systems. The Development of a Flight Control System Simulator, Research on a Control Surface Flutter Suppression Technique and High Temperature Testing of Mil-H-83282

Abstract

This report presents the results of the following three research and development activities: the design, fabrication and test of a multi-channel flight control system hybrid simulator; the analysis and application of a flutter damping technique for hydraulically actuated slab type control surfaces; and the experimental testing of Mil-H-83282 hydraulic fluid in a pumping system at elevated temperature.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1975
Accession Number
ADA014367

Entities

People

  • Gavin D. Jenney

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Human Systems

DTIC Thesaurus Topics

  • Computer Programs
  • Computers
  • Control Panels
  • Control Simulators
  • Control Surfaces
  • Control Systems
  • Damage Detection
  • Equations Of Motion
  • Flight Control Systems
  • Frequency Response
  • High Temperature
  • Junction Boxes
  • Measurement
  • Military Aircraft
  • Resonant Frequency
  • Simulators
  • Transducers

Fields of Study

  • Physics

Readers

  • Petroleum Engineering
  • Robotics and Automation.
  • Software Engineering