Volume 113 Issue 1 | J. Eng. Gas Turbines Power

Research Papers

On the Leading Edge: Combining Maturity and Advanced Technology on the F404 Turbofan Engine

S. F. Powel, IV

J. Eng. Gas Turbines Power. January 1991, 113(1): 1–10. doi: https://doi.org/10.1115/1.2906525

View articletitled, On the Leading Edge: Combining Maturity and Advanced Technology on the F404 Turbofan Engine

Topics: Engines , Turbofans , Design , Knudsen number , Aircraft engines , Blocks (Building materials) , Exhaust systems , Fibers , Flight , Nozzles

Engine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft

R. W. Cue, D. E. Muir

J. Eng. Gas Turbines Power. January 1991, 113(1): 11–19. doi: https://doi.org/10.1115/1.2906519

Abstract

View articletitled, Engine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft

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Topics: Aircraft , Engines , Maintenance , Flight , Computer software , Condition monitoring

SNECMA M88 Engine Development Status

J. C. Corde

J. Eng. Gas Turbines Power. January 1991, 113(1): 20–24. doi: https://doi.org/10.1115/1.2906526

Abstract

View articletitled, SNECMA M88 Engine Development Status

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Topics: Engines , Flight

EJ200—The Engine for the New European Fighter Aircraft

R. J. Lane, J. Behenna

J. Eng. Gas Turbines Power. January 1991, 113(1): 25–32. doi: https://doi.org/10.1115/1.2906527

Abstract

View articletitled, EJ200—The Engine for the New European Fighter Aircraft

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Topics: Aircraft , Engines , Design , Collaboration

Advanced Technology Programs for Small Turboshaft Engines: Past, Present, Future

E. T. Johnson, H. Lindsay

J. Eng. Gas Turbines Power. January 1991, 113(1): 33–39. doi: https://doi.org/10.1115/1.2906528

Abstract

View articletitled, Advanced Technology Programs for Small Turboshaft Engines: Past, Present, Future

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Topics: Engines , Aircraft engines , Aircraft propulsion , Army , Aviation , Gas turbines , Generators , NASA , US Department of Defense

Computational Fluid Dynamic Applications for Jet Propulsion System Integration

R. H. Tindell

J. Eng. Gas Turbines Power. January 1991, 113(1): 40–50. doi: https://doi.org/10.1115/1.2906529

Abstract

View articletitled, Computational Fluid Dynamic Applications for Jet Propulsion System Integration

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Topics: Computational fluid dynamics , Jet propulsion , Flow (Dynamics) , Aircraft , Design , Nozzles , Diffusers , Engineers , Flight , Fluid mechanics

Airframe/Propulsion Integration at Transonic Speeds

W. P. Henderson

J. Eng. Gas Turbines Power. January 1991, 113(1): 51–59. doi: https://doi.org/10.1115/1.2906530

Abstract

View articletitled, Airframe/Propulsion Integration at Transonic Speeds

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Topics: Aircraft , Mach number , NASA , Nozzles , Propellers , Propulsion , Propulsion systems , Thrust , Tunnels , Turbofans

Integrated Propulsion System Requirements for Control of STOVL Aircraft

G. W. Gallops, C. F. Weiss, R. A. Carlton

J. Eng. Gas Turbines Power. January 1991, 113(1): 60–67. doi: https://doi.org/10.1115/1.2906531

Abstract

View articletitled, Integrated Propulsion System Requirements for Control of STOVL Aircraft

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Topics: Aircraft , Propulsion systems , Engines , Dynamic response , Degrees of freedom , Flight , Jets , Nozzles , Propulsion , Simulation

STOVL Hot Gas Ingestion Control Technology

K. C. Amuedo, B. R. Williams, J. D. Flood, A. L. Johns

J. Eng. Gas Turbines Power. January 1991, 113(1): 68–74. doi: https://doi.org/10.1115/1.2906532

Abstract

View articletitled, STOVL Hot Gas Ingestion Control Technology

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Topics: Aircraft , Control systems , Engines , NASA , Nozzles , Temperature , Testing , Wind tunnels

Introduction to the Basic Technology of Stealth Aircraft: Part 1—Basic Considerations and Aircraft Self-Emitted Signals (Passive Considerations)

D. Howe

J. Eng. Gas Turbines Power. January 1991, 113(1): 75–79. doi: https://doi.org/10.1115/1.2906533

Abstract

View articletitled, Introduction to the Basic Technology of Stealth Aircraft: Part 1—Basic Considerations and Aircraft Self-Emitted Signals (Passive Considerations)

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Topics: Aircraft , Signals , Emissions , Acoustics , Design

Introduction to the Basic Technology of Stealth Aircraft: Part 2—Illumination by the Enemy (Active Considerations)

D. Howe

J. Eng. Gas Turbines Power. January 1991, 113(1): 80–86. doi: https://doi.org/10.1115/1.2906534

Abstract

View articletitled, Introduction to the Basic Technology of Stealth Aircraft: Part 2—Illumination by the Enemy (Active Considerations)

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Topics: Aircraft , Radar , Design , Probability

Optimizing Aircraft Performance With Adaptive, Integrated Flight/Propulsion Control

R. H. Smith, J. D. Chisholm, J. F. Stewart

J. Eng. Gas Turbines Power. January 1991, 113(1): 87–94. doi: https://doi.org/10.1115/1.2906535

Abstract

View articletitled, Optimizing Aircraft Performance With Adaptive, Integrated Flight/Propulsion Control

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Topics: Aircraft , Flight , Propulsion , Engines , Thrust , Algorithms , Control algorithms , Fuel consumption , Aircraft engines , Cycles

Simulation of Aircraft Gas Turbine Engines

I. H. Ismail, F. S. Bhinder

J. Eng. Gas Turbines Power. January 1991, 113(1): 95–99. doi: https://doi.org/10.1115/1.2906536

Abstract

View articletitled, Simulation of Aircraft Gas Turbine Engines

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Topics: Aircraft , Gas turbines , Simulation , Computer software , Engines , Performance characterization , Steady state

Determination of Cycle Configuration of Gas Turbines and Aircraft Engines by an Optimization Procedure

Y. Tsujikawa, M. Nagaoka

J. Eng. Gas Turbines Power. January 1991, 113(1): 100–105. doi: https://doi.org/10.1115/1.2906515

Abstract

View articletitled, Determination of Cycle Configuration of Gas Turbines and Aircraft Engines by an Optimization Procedure

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Topics: Aircraft engines , Cycles , Gas turbines , Optimization , Impulse (Physics) , Scramjets , Thermal efficiency , Thrust

A New Method of Predicting the Performance of Gas Turbine Engines

Wang Yonghong

J. Eng. Gas Turbines Power. January 1991, 113(1): 106–111. doi: https://doi.org/10.1115/1.2906516

Abstract

View articletitled, A New Method of Predicting the Performance of Gas Turbine Engines

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Topics: Gas turbines , Algorithms , Computation , Turbines , Dimensions , Stability

An Algorithm and Criteria for Compressor Characteristics Real Time Modeling and Approximation

A. M. El-Gammal

J. Eng. Gas Turbines Power. January 1991, 113(1): 112–118. doi: https://doi.org/10.1115/1.2906517

Abstract

View articletitled, An Algorithm and Criteria for Compressor Characteristics Real Time Modeling and Approximation

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Topics: Algorithms , Approximation , Compressors , Modeling , Engines , Aircraft engines , Simulation

3-D Laser Anemometer Measurements in a Labyrinth Seal

G. L. Morrison, M. C. Johnson, G. B. Tatterson

J. Eng. Gas Turbines Power. January 1991, 113(1): 119–125. doi: https://doi.org/10.1115/1.2906518

Abstract

View articletitled, 3-D Laser Anemometer Measurements in a Labyrinth Seal

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Topics: Lasers , Cavities , Flow (Dynamics) , Clearances (Engineering) , Stress , Stress tensors

The Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow

V. Scherer, S. Wittig

J. Eng. Gas Turbines Power. January 1991, 113(1): 126–134. doi: https://doi.org/10.1115/1.2906520

Abstract

View articletitled, The Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow

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Topics: Convection , Flow (Dynamics) , Heat transfer , Finite volume methods , Laser Doppler anemometry , Momentum , Pressure , Reynolds number

Thermal Barrier Characteristics of Partially Stabilized Zirconia Coatings on INCOLOY Alloy 909 (A Controlled Expansion Alloy)

G. D. Smith

J. Eng. Gas Turbines Power. January 1991, 113(1): 135–139. doi: https://doi.org/10.1115/1.2906521

Abstract

View articletitled, Thermal Barrier Characteristics of Partially Stabilized Zirconia Coatings on INCOLOY Alloy 909 (A Controlled Expansion Alloy)

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Topics: Alloys , Coatings , Temperature , Metals , Flow (Dynamics) , Oxidation , Ceramics , Cooling , Gas turbines , Heat

Application of HOST Technology to the SSME HPFTP Blade

R. L. McKnight, T. S. Cook, G. S. Bechtel, H. T. Huang

J. Eng. Gas Turbines Power. January 1991, 113(1): 140–144. doi: https://doi.org/10.1115/1.2906522

Abstract

View articletitled, Application of HOST Technology to the SSME HPFTP Blade

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Topics: Blades , Structural analysis , Design , Heat transfer , Advanced materials , Aircraft , Coatings , Constitutive equations , Databases , Engines

A Computer Code Using Exergy for Optimizing Thermal Plants

G. Bidini, S. S. Stecco

J. Eng. Gas Turbines Power. January 1991, 113(1): 145–150. doi: https://doi.org/10.1115/1.2906523

Abstract

View articletitled, A Computer Code Using Exergy for Optimizing Thermal Plants

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Topics: Computers , Energy conservation , Exergy , Fluids , Heat , Heat transfer , Industrial plants , Systems analysis , Temperature

A GCC Power Plant With Methanol Storage for Intermediate-Load Duty

J. A. Paffenbarger

J. Eng. Gas Turbines Power. January 1991, 113(1): 151–157. doi: https://doi.org/10.1115/1.2906524

Abstract

View articletitled, A GCC Power Plant With Methanol Storage for Intermediate-Load Duty

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Topics: Methanol , Power stations , Storage , Stress , Coal , Design , Fuels , Combined cycle power stations , Combined cycles , Electric power generation

Research Papers

On the Leading Edge: Combining Maturity and Advanced Technology on the F404 Turbofan Engine

Engine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft

SNECMA M88 Engine Development Status

EJ200—The Engine for the New European Fighter Aircraft

Advanced Technology Programs for Small Turboshaft Engines: Past, Present, Future

Computational Fluid Dynamic Applications for Jet Propulsion System Integration

Airframe/Propulsion Integration at Transonic Speeds

Integrated Propulsion System Requirements for Control of STOVL Aircraft

STOVL Hot Gas Ingestion Control Technology

Introduction to the Basic Technology of Stealth Aircraft: Part 1—Basic Considerations and Aircraft Self-Emitted Signals (Passive Considerations)

Introduction to the Basic Technology of Stealth Aircraft: Part 2—Illumination by the Enemy (Active Considerations)

Optimizing Aircraft Performance With Adaptive, Integrated Flight/Propulsion Control

Simulation of Aircraft Gas Turbine Engines

Determination of Cycle Configuration of Gas Turbines and Aircraft Engines by an Optimization Procedure

A New Method of Predicting the Performance of Gas Turbine Engines

An Algorithm and Criteria for Compressor Characteristics Real Time Modeling and Approximation

3-D Laser Anemometer Measurements in a Labyrinth Seal

The Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow

Thermal Barrier Characteristics of Partially Stabilized Zirconia Coatings on INCOLOY Alloy 909 (A Controlled Expansion Alloy)

Application of HOST Technology to the SSME HPFTP Blade

A Computer Code Using Exergy for Optimizing Thermal Plants

A GCC Power Plant With Methanol Storage for Intermediate-Load Duty

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