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Dynamic neural network-based fault diagnosis of gas turbine engines

Neurocomputing (Amsterdam), 2014-02, Vol.125, p.153-165

2014

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Bayesian Hierarchical Models for aerospace gas turbine engine prognostics

Expert systems with applications, 2015-01, Vol.42 (1), p.539-553

2015

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Tool wear characteristics in machining of nickel-based superalloys

International journal of machine tools & manufacture, 2013-01, Vol.64, p.60-77

2013

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A novel method for the optimal band selection for vibration signal demodulation and comparison with the Kurtogram

Mechanical systems and signal processing, 2011, Vol.25 (1), p.431-451

2011

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Newton-Like Extremum-Seeking for the Control of Thermoacoustic Instability

IEEE transactions on automatic control, 2010-09, Vol.55 (9), p.2094-2105

2010

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Large-eddy simulation and experimental study of heat transfer, nitric oxide emissions and combustion instability in a swirled turbulent high-pressure burner

Journal of fluid mechanics, 2007-01, Vol.570, p.17-46

2007

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Physical and chemical characterization of SIDI engine particulates

Combustion and flame, 2013-11, Vol.160 (11), p.2517-2528

2013

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A Method for Handling Uncertainty in Evolutionary Optimization With an Application to Feedback Control of Combustion

IEEE transactions on evolutionary computation, 2009-02, Vol.13 (1), p.180-197

2009

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Two-dimensional modeling of an aircraft engine structural bladed disk-casing modal interaction

Journal of sound and vibration, 2009-01, Vol.319 (1), p.366-391

2009

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A multi-regulator sliding mode control strategy for output-constrained systems

Automatica (Oxford), 2011-10, Vol.47 (10), p.2251-2259

Richter, Hanz

2011

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Modeling of a rotor speed transient response with radial rubbing

Journal of sound and vibration, 2010-03, Vol.329 (5), p.527-546

2010

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Response surface approximation of Pareto optimal front in multi-objective optimization

Computer methods in applied mechanics and engineering, 2007, Vol.196 (4), p.879-893

2007

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Experimental investigation of droplet size influence on low pressure steam turbine blade erosion

Wear, 2013-06, Vol.303 (1-2), p.83-86

2013

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Development of high intensity CDC combustor for gas turbine engines

Applied energy, 2011-03, Vol.88 (3), p.963-973

2011

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Full three-dimensional investigation of structural contact interactions in turbomachines

Journal of sound and vibration, 2012-05, Vol.331 (11), p.2578-2601

2012

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Use of a Ni60Ti shape memory alloy for active jet engine chevron application: II. Experimentally validated numerical analysis

Smart materials and structures, 2010-01, Vol.19 (1), p.015021-015021 (18)

2010

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Optimal design of aeroengine turbine disc based on kriging surrogate models

Computers & structures, 2011, Vol.89 (1), p.27-37

2011

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Gas turbine performance prognostic for condition-based maintenance

Applied energy, 2009-10, Vol.86 (10), p.2152-2161

2009

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Use of a Ni60Ti shape memory alloy for active jet engine chevron application: I. Thermomechanical characterization

Smart materials and structures, 2010-01, Vol.19 (1), p.015020-015020 (14)

2010

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Polynomial LPV synthesis applied to turbofan engines

Control engineering practice, 2010-09, Vol.18 (9), p.1077-1083

2010

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The hypersonic environment: Required operating conditions and design challenges

Journal of materials science, 2004-10, Vol.39 (19), p.5915-5924

2004

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Design and testing of a deformable wind turbine blade control surface

Smart materials and structures, 2012-10, Vol.21 (10), p.105019-1-10

2012

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Performance and emission characteristics of biofuel in a small-scale gas turbine engine

Applied energy, 2010-05, Vol.87 (5), p.1701-1709

2010

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Multi-objective optimization of turbomachinery using improved NSGA-II and approximation model

Computer methods in applied mechanics and engineering, 2011-02, Vol.200 (9), p.883-895

2011

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LES of an ignition sequence in a gas turbine engine

Combustion and flame, 2008-07, Vol.154 (1), p.2-22

2008

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Dynamic neural network-based fault diagnosis of gas turbine engines

Bayesian Hierarchical Models for aerospace gas turbine engine prognostics

Tool wear characteristics in machining of nickel-based superalloys

A novel method for the optimal band selection for vibration signal demodulation and comparison with the Kurtogram

Newton-Like Extremum-Seeking for the Control of Thermoacoustic Instability

Large-eddy simulation and experimental study of heat transfer, nitric oxide emissions and combustion instability in a swirled turbulent high-pressure burner

Physical and chemical characterization of SIDI engine particulates

A Method for Handling Uncertainty in Evolutionary Optimization With an Application to Feedback Control of Combustion

Two-dimensional modeling of an aircraft engine structural bladed disk-casing modal interaction

A multi-regulator sliding mode control strategy for output-constrained systems

Modeling of a rotor speed transient response with radial rubbing

Response surface approximation of Pareto optimal front in multi-objective optimization

Experimental investigation of droplet size influence on low pressure steam turbine blade erosion

Development of high intensity CDC combustor for gas turbine engines

Full three-dimensional investigation of structural contact interactions in turbomachines

Use of a Ni60Ti shape memory alloy for active jet engine chevron application: II. Experimentally validated numerical analysis

Optimal design of aeroengine turbine disc based on kriging surrogate models

Gas turbine performance prognostic for condition-based maintenance

Use of a Ni60Ti shape memory alloy for active jet engine chevron application: I. Thermomechanical characterization

Polynomial LPV synthesis applied to turbofan engines

The hypersonic environment: Required operating conditions and design challenges

Design and testing of a deformable wind turbine blade control surface

Performance and emission characteristics of biofuel in a small-scale gas turbine engine

Multi-objective optimization of turbomachinery using improved NSGA-II and approximation model

LES of an ignition sequence in a gas turbine engine

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