Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems.
Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,
NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
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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
- Fluidics and Fluerics
- Jet and Gas Turbine Engines