FLIGHT TEST OF A HONEYWELL, INC., FLUIDIC YAW DAMPER

Abstract

Flight tests were conducted to evaluate the performance and feasibility of a fluidic yaw damper system. A standard UH-1C helicopter was used as a test vehicle.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1968
Accession Number
AD0674211

Entities

People

  • John C. Kidwell

Organizations

  • Bell Flight

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Actuators
  • Aerodynamic Configurations
  • Aircraft Cabins
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Army Aviation
  • Control Panels
  • Control Systems
  • Environment
  • Helicopters
  • Insensitive Explosives
  • Instrumentation
  • Level Flight
  • Measurement
  • Stabilization Systems
  • Standards

Readers

  • Aerospace Test and Evaluation
  • Robotics and Automation.