Accession Number:

AD0694111

Title:

FLUIDIC CONTROL SYSTEMS FOR AEROSPACE PROPULSION.

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1969-09-01

Pagination or Media Count:

156.0

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

Descriptors:

• *RAMJET ENGINES
• *GAS TURBINES
• CONTROL SYSTEMS
• CONTROL SYSTEMS
• FLUID AMPLIFIERS
• FLUIDICS
• STATE OF THE ART
• REPORTS
• DETECTORS
• COANDA EFFECT
• SERVOAMPLIFIERS
• FREQUENCY CONVERTERS
• ADIABATIC GAS FLOW
• TEMPERATURE SENSITIVE ELEMENTS
• LIQUID LEVEL CONTROL
• REPORTS

Subject Categories:

• Fluidics and Fluerics
• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE