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E. H. James
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Proceedings Papers

Combustion Modelling to Evaluate Turbulent Burning Velocities During Spark Ignition Engine Combustion

E. H. James
Proc. ASME. CIE91, ASME 1991 Computers in Engineering Conference: Volume 2 — Finite Elements/Computational Geometry; Computers in Education; Robotics and Controls, 375, August 18–22, 1991
Publisher: American Society of Mechanical Engineers
Paper No: CIE1991-0141
https://doi.org/10.1115/CIE1991-0141
View Paper titled, Combustion Modelling to Evaluate Turbulent Burning Velocities During Spark Ignition Engine Combustion
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Topics: Combustion, Modeling, Spark-ignition engine, Turbulence, Flames, Computers, Combustion chambers, Emissions, Engines, Exhaust systems
Proceedings Papers

Boundary Layer Profile Investigations Downstream of an Aero-Engine Intake Anti-Icing Air Exhaust Slot

S. J. Downs, E. H. James
Proc. ASME. GT1987, Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery, V002T02A012, May 31–June 4, 1987
Publisher: American Society of Mechanical Engineers
Paper No: 87-GT-237
https://doi.org/10.1115/87-GT-237
View Paper titled, Boundary Layer Profile Investigations Downstream of an Aero-Engine Intake Anti-Icing Air Exhaust Slot
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Topics: Aircraft engines, Boundary layers, Exhaust systems, Engines, Air flow, Sprays, Turbulence, Water, Wind tunnels
Proceedings Papers

Investigations Relating to the Effects of Various Internal Geometries on the Effectiveness of an Aero-Engine Intake Thermal Anti-Icing System

S. J. Riley, E. H. James
Proc. ASME. GT1994, Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, V004T09A042, June 13–16, 1994
Publisher: American Society of Mechanical Engineers
Paper No: 94-GT-276
https://doi.org/10.1115/94-GT-276
View Paper titled, Investigations Relating to the Effects of Various Internal Geometries on the Effectiveness of an Aero-Engine Intake Thermal Anti-Icing System
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Topics: Aircraft engines, Design, Geometry, Ice, Flow (Dynamics), Maintenance, Pipes, Reliability, Temperature, Weight (Mass)
Proceedings Papers

The Influence of Various Exhaust Geometrical Parameters on the Effectiveness of an Aero-Engine Intake Thermal Anti-Icing System

S. J. Riley, E. H. James
Proc. ASME. GT1994, Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, V004T09A041, June 13–16, 1994
Publisher: American Society of Mechanical Engineers
Paper No: 94-GT-275
https://doi.org/10.1115/94-GT-275
View Paper titled, The Influence of Various Exhaust Geometrical Parameters on the Effectiveness of an Aero-Engine Intake Thermal Anti-Icing System
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Topics: Aircraft engines, Exhaust systems, Heating, Acoustics, Compressors, Engines, Geometry, Ice, Maintenance, Manufacturing
Journal Articles

Radiative Heat Transfer Calculations in Three-Dimensional Complex Geometries

W. M. G. Malalasekera, E. H. James
Journal: ASME Journal of Heat and Mass Transfer
Publisher: ASME
Article Type: Technical Briefs
J. Heat Mass Transfer. February 1996, 118(1): 225–228.
https://doi.org/10.1115/1.2824045
Published Online: February 1, 1996
View Article titled, Radiative Heat Transfer Calculations in Three-Dimensional Complex Geometries
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Topics: Combustion chambers, Furnaces, Numerical analysis, Radiation (Physics), Radiative heat transfer