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AD852757

Publication Date	1968
Personal Author	Wolfshagen, R. G.; Ogura, I. A.
Page 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)
Keywords	Turbojet engines Detectors Servomechanisms Synchros Probes Fluidics Fluid amplifiers Temperature Pressure Angle of attack Acceleration Reliability Piezoelectric effect Planning Transients
Source Agency	Non Paid Delimited ADS
NTIS Subject Category	94I - Hydraulic & Pneumatic Equipment 81D - Jet & Gas Turbine Engines
Corporate Authors	North American Rockwell Corp Los Angeles Calif Los Angeles Div
Supplemental Notes	See also Rept. no. C8-1638/301-V0l-2, AD-852 758. Prepared in cooperation with Northern Research and Engineering Corp., Cambridge, Mass., General Motors Corp., Indianapolis, Ind., Allison Div., and Pratt and Whitney Aircraft, East Hartford, Conn.
Document Type	Technical Report
Title Note	Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1.
NTIS Issue Number	197701
Contract Number	F33615-67-C-1848

Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems.

Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems.
AD852757

Publication Date	1968
Personal Author	Wolfshagen, R. G.; Ogura, I. A.
Page 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)
Keywords	Turbojet engines Detectors Servomechanisms Synchros Probes Fluidics Fluid amplifiers Temperature Pressure Angle of attack Acceleration Reliability Piezoelectric effect Planning Transients
Source Agency	Non Paid Delimited ADS
NTIS Subject Category	94I - Hydraulic & Pneumatic Equipment 81D - Jet & Gas Turbine Engines
Corporate Authors	North American Rockwell Corp Los Angeles Calif Los Angeles Div
Supplemental Notes	See also Rept. no. C8-1638/301-V0l-2, AD-852 758. Prepared in cooperation with Northern Research and Engineering Corp., Cambridge, Mass., General Motors Corp., Indianapolis, Ind., Allison Div., and Pratt and Whitney Aircraft, East Hartford, Conn.
Document Type	Technical Report
Title Note	Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1.
NTIS Issue Number	197701
Contract Number	F33615-67-C-1848