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Influence of In-Flight LOX Collection Upon Ramjet Performances
In-Flight LOX Collection TSTO with Different Separation Mach Numbers
Research on Small Turbojet Engines
INFLUENCE OF THE TURBOSHAFT DESIGN POINT ON ITS INSTALLED PERFORMANCE IN A HELICOPTER
A FUEL CELL PROPULSION SYSTEM FOR A MINI-UAV
AIAA-2005-1271 NUMERICAL SIMULATIONS IN THE DESIGN OF A COMBUSTION CHAMBER FOR A MICRO GAS TURBINE
AIAA-2005-1212 HYDROGEN AS AN (AERO) GAS TURBINE FUEL
AIAA-2007-1170 DEVELOPMENT OF A COMBUSTION CHAMBER FOR AN ULTRA MICRO GAS TURBINE
Developing a European Research Strategy in the High Altitude Aircraft and Airship Sector
Comparison of Propulsion Technologies for a HALE Airship
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
Improved Performance Assessment of a Precooled Turbofan for Hypersonic Vehicle Acceleration
Hydrogen Fueled Precooled Airbreathing Engines for Hypersonic Aircraft and Spaceplanes
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
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
Testing of Carbon Brush Seals for Aero-Engine Bearing Chambers
Experimental Analysis of the Performances of Oil Filters in Aero Engines
Experimental Study of an Air-Oil Pump and Separator Solution