Accession Number : AD0852757
Title : Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems.
Descriptive Note : Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,
Corporate Author : NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
Personal Author(s) : Wolfshagen, Ronald G. ; Ogura, Isaac A.
Report Date : DEC 1968
Pagination or Media Count : 134
Abstract : This part describes the results of a survey conducted to determine the present and the estimated 1970 capabilities of sensors applicable to the control of aircraft propulsion systems. The survey included electromechanical and fluid amplifier (fluidic) sensors for measurement of gas dynamic and static properties as well as for measurement of airframe dynamic parameters. (Author)
Descriptors : (*TURBOJET ENGINES, DETECTORS), SERVOMECHANISMS, SYNCHROS, PROBES, FLUIDICS, FLUID AMPLIFIERS, TEMPERATURE, PRESSURE, ANGLE OF ATTACK, ACCELERATION, RELIABILITY, PIEZOELECTRIC EFFECT, PLANNING, TRANSIENTS.
Subject Categories : Fluidics and Fluerics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE