FLUIDIC CONTROL SYSTEMS FOR AEROSPACE PROPULSION.

Abstract

This document is intended as a progress report on fluidics as applied to aerospace propulsion problems. After a minimal review of basic operating principles, a number of operating prototype sensors and control systems will be described. Fluidic control systems for aerodynamic inlets, gas turbines, and rocket engines will be treated. Some of these systems have functioned successfully at temperatures exceeding 3000 Kelvin. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1969
Accession Number
AD0694111

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Control Systems
  • Engines
  • Fluid Control
  • Fluidics
  • Gas Turbines
  • Prototypes
  • Rocket Engines
  • Rockets
  • Turbines

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Robotics and Automation.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster