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Influence of Inlet Piping Conditions on Pump Performance in an Aircraft Engine Lubrication System
Development and Testing of Advanced Surface Oil Coolers for Aero Engines
Experimental Analysis of the Performances of Oil Filters in Aero Engines
Testing of Carbon Brush Seals for Aero-Engine Bearing Chambers
Improved Performance Assessment of a Precooled Turbofan for Hypersonic Vehicle Acceleration
Hydrogen Fueled Precooled Airbreathing Engines for Hypersonic Aircraft and Spaceplanes
Experimental Study of an Air-Oil Pump and Separator Solution
Mathematical Model of Brush Seal - A Nonlinear Analytical Solution
Study of Air-Oil Separation and Pumping Devices for Gas Turbine Engines
Development and Testing of Advanced Surface Coolers for Aero Engines
Research on Small Turbojet Engines
LES OF JETS-IN-CROSS-FLOW AND APPLICATION TO THE ``MICROMIX'' HYDROGEN COMBUSTION
UNCONVENTIONAL TURBOFAN ENGINES BURNING HYDROGEN
TWO-PHASE FLOW PUMP AND SEPARATOR SYSTEM : EXPERIMENTAL AND NUMERICAL STUDY
Influence of In-Flight LOX Collection Upon Ramjet Performances
In-Flight LOX Collection TSTO with Different Separation Mach Numbers
AIAA-2007-1170 DEVELOPMENT OF A COMBUSTION CHAMBER FOR AN ULTRA MICRO GAS TURBINE