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Intelligent Control of the F-100 Turbofan Engine for Full Flight Envelope Operation
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Shih-Tin Lin,
Published/Copyright:
December 1, 2005
Published Online: 2005-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Intelligent Control of the F-100 Turbofan Engine for Full Flight Envelope Operation
- Numerical Study of Three-Dimensional Jets Using Point Source Method
- Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice
- Numerical Simulation of Cold Flow in Axisymmetric Dump Combustor
- Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine
- Performance of Isolator Fed by Laval Nozzle
- A New Numerical Approach to Two-Dimensional Stefan Problem
- Axial Fan Efficiency: A New Design Approach
Articles in the same Issue
- CONTENTS
- Intelligent Control of the F-100 Turbofan Engine for Full Flight Envelope Operation
- Numerical Study of Three-Dimensional Jets Using Point Source Method
- Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice
- Numerical Simulation of Cold Flow in Axisymmetric Dump Combustor
- Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine
- Performance of Isolator Fed by Laval Nozzle
- A New Numerical Approach to Two-Dimensional Stefan Problem
- Axial Fan Efficiency: A New Design Approach
