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)
Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems
1968
134 pages
Report
No indication
English
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