Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring

J.D. Disbrow,; E.L. Duke,; R.J. Ray,

doi:10.1515/TJJ.1992.9.4.267

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Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring

J.D. Disbrow, , E.L. Duke, and R.J. Ray,

Published/Copyright: December 1, 1992

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From the journal International Journal of Turbo and Jet Engines Volume 9 Issue 4

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Vancouver

Disbrow,, J.D., Duke,, E.L. and Ray,, R.J.. "Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring" International Journal of Turbo and Jet Engines, vol. 9, no. 4, pp. 267-276. https://doi.org/10.1515/TJJ.1992.9.4.267

Disbrow,, J., Duke,, E. & Ray,, R. (). Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring. International Journal of Turbo and Jet Engines, 9(4), 267-276. https://doi.org/10.1515/TJJ.1992.9.4.267

Disbrow,, J., Duke,, E. and Ray,, R. () Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring. International Journal of Turbo and Jet Engines, Vol. 9 (Issue 4), pp. 267-276. https://doi.org/10.1515/TJJ.1992.9.4.267

Disbrow,, J.D., Duke,, E.L. and Ray,, R.J.. "Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring" International Journal of Turbo and Jet Engines 9, no. 4 (): 267-276. https://doi.org/10.1515/TJJ.1992.9.4.267

Disbrow, J, Duke, E, Ray, R. Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring. International Journal of Turbo and Jet Engines. ;9(4): 267-276. https://doi.org/10.1515/TJJ.1992.9.4.267

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Published Online: 1992-12

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Articles in the same Issue

CONTENTS
Experimental Determination of Prewhirl Effects on Centrifugal Compressor Internal Aerodynamics
Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring
Minimization of the Number of Cooling Holes in Internally Cooled Turbine Blades
A Computational Study of Gas Turbine Combustion Chamber Flow Field
Effects of Length and Configuration of Transverse Discrete Ribs on Heat Transfer and Friction for Turbulent Flow in a Square Channel
Gas Turbine Axial Compressor Fouling: A Unified Treatment of its Effects, Detection, and Control

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https://doi.org/10.1515/TJJ.1992.9.4.267

Articles in the same Issue

CONTENTS
Experimental Determination of Prewhirl Effects on Centrifugal Compressor Internal Aerodynamics
Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring
Minimization of the Number of Cooling Holes in Internally Cooled Turbine Blades
A Computational Study of Gas Turbine Combustion Chamber Flow Field
Effects of Length and Configuration of Transverse Discrete Ribs on Heat Transfer and Friction for Turbulent Flow in a Square Channel
Gas Turbine Axial Compressor Fouling: A Unified Treatment of its Effects, Detection, and Control