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)
Fluidic Control Systems for Aerospace Propulsion
1969
156 pages
Report
Keine Angabe
Englisch
Hydraulic & Pneumatic Equipment , Jet & Gas Turbine Engines , Ramjet engines , Control systems , Gas turbines , Fluid amplifiers , Fluidics , State-of-the-art reviews , Sensors , Coanda effect , Servo amplifiers , Frequency converters , Adiabatic gas flow , Temperature sensitive elements , Liquid level control , Reports , Fluerics , Fluidic transmission lines , Proportional amplifiers