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turbofan engines

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View A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics By Takahisa Kobayashi

A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics

A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics

By Takahisa Kobayashi

View The WINCOF-I code By S. N. B. Murthy

The WINCOF-I code

The WINCOF-I code

By S. N. B. Murthy

View Real-time simulation of an F110/STOVL turbofan engine By Colin K. Drummond

Real-time simulation of an F110/STOVL turbofan engine

Real-time simulation of an F110/STOVL turbofan engine

By Colin K. Drummond

View Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine By James T. Walton

Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine

Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine

By James T. Walton

View Wave rotor-enhanced gas turbine engines By Gerard E. Welch

Wave rotor-enhanced gas turbine engines

Wave rotor-enhanced gas turbine engines

By Gerard E. Welch

View Ultra-efficient engine diameter study By D. L. Daggett

Ultra-efficient engine diameter study

Ultra-efficient engine diameter study

By D. L. Daggett

View Advanced control of turbofan engines By Hanz Richter
Cover of Advanced control of turbofan engines by hanz richter

Advanced control of turbofan engines

By Hanz Richter

View Computation of noise radiation from turbofans By M. Nallasamy

Computation of noise radiation from turbofans

Computation of noise radiation from turbofans

By M. Nallasamy

View Influence of vane sweep on rotor-stator interaction noise By Edmane Envia

Influence of vane sweep on rotor-stator interaction noise

Influence of vane sweep on rotor-stator interaction noise

By Edmane Envia

View A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine By Duane L. Mattern

A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine

A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine

By Duane L. Mattern

View A preliminary evaluation of an F100 engine parameter estimation process using flight data By Trindel A. Maine

A preliminary evaluation of an F100 engine parameter estimation process using flight data

A preliminary evaluation of an F100 engine parameter estimation process using flight data

By Trindel A. Maine

View A microprocessor-based real-time simulator of a turbofan engine By Jonathan S. Litt

A microprocessor-based real-time simulator of a turbofan engine

A microprocessor-based real-time simulator of a turbofan engine

By Jonathan S. Litt

View A real-time simulation evaluation of an advanced detection, isolation and accommodation algorithm for sensor failures in turbine engines By Walter C. Merrill

A real-time simulation evaluation of an advanced detection, isolation and accommodation algorithm for sensor failures in turbine engines

A real-time simulation evaluation of an advanced detection, isolation and accommodation algorithm for sensor failures in turbine engines

By Walter C. Merrill

View NOx emission reduction in commercial jets through water injection By Vladimir Balepin

NOx emission reduction in commercial jets through water injection

NOx emission reduction in commercial jets through water injection

By Vladimir Balepin

View Full flight envelope direct thrust measurement on a supersonic aircraft By Timothy R. Conners

Full flight envelope direct thrust measurement on a supersonic aircraft

Full flight envelope direct thrust measurement on a supersonic aircraft

By Timothy R. Conners

View The Air Force and the great engine war By Robert W. Drewes
Cover of The Air Force and the great engine war by robert w. drewes

The Air Force and the great engine war

By Robert W. Drewes

View Experimental performance and combustion-stability of a full-scale duct burner for a supersonic turbofan engine By J. Robert Branstetter

Experimental performance and combustion-stability of a full-scale duct burner for a supersonic turbofan engine

Experimental performance and combustion-stability of a full-scale duct burner for a supersonic turbofan engine

By J. Robert Branstetter

View Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation By Boeing Company.

Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation

Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation

By Boeing Company.

View Alternatives for linear multivariable control with turbofan engine theme problem By International Forum on Alternatives for Linear Multivariable Control (1977 Chicago, Ill.)

Alternatives for linear multivariable control with turbofan engine theme problem

Alternatives for linear multivariable control with turbofan engine theme problem

By International Forum on Alternatives for Linear Multivariable Control (1977 Chicago, Ill.)

View Inlet shape effects on the far-field sound of a model fan By L. R. Clark

Inlet shape effects on the far-field sound of a model fan

Inlet shape effects on the far-field sound of a model fan

By L. R. Clark

View Small Engine Technology (SET) By Max J. Miller

Small Engine Technology (SET)

Small Engine Technology (SET)

By Max J. Miller

View A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring By Steven A. Johnson

A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring

A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring

By Steven A. Johnson

View An educational introduction to transonic compressor stage design principles By Philip G. Hill

An educational introduction to transonic compressor stage design principles

An educational introduction to transonic compressor stage design principles

By Philip G. Hill

View Type certification basis for conversion from reciprocating engine to turbine engine-powered part 23 airplanes By United States Federal Aviation Administration

Type certification basis for conversion from reciprocating engine to turbine engine-powered part 23 airplanes

Type certification basis for conversion from reciprocating engine to turbine engine-powered part 23 airplanes

By United States Federal Aviation Administration