FLUIDIC CONTROL SYSTEMS FOR AEROSPACE PROPULSION.

FLUIDIC CONTROL SYSTEMS FOR AEROSPACE PROPULSION.

Active / Technical Report | Accession Number: AD0694111 |

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

Author(s):

No Author(s) Identified

Author Organization(s):

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Supplementary Note:

NATO furnished.

Pagination:

0156

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

AGARD-ograph-135, AGARD-Lecture Ser 35

Subject Terms

Joint Capability Areas:

JCA_3.2_Engagement; JCA_3_Force Application

Communities of Interest:

Weapons Technologies

Descriptor(s):

*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

Field(s)/Group(s):

Fluidics and Fluerics, Jet and Gas Turbine Engines

Keyword(s):

*FLUERICS, AMPLIFIERS

Report Date:

1969 Sep 01