Rotor dynamic analysis and bearing optimization study of a 3800 hp steam turbine...4.0 inches on the inlet and exhaust ends, respectively....
Development of a floating piston expander control algorithm for a collins-type cryocooler by... This pressure distribution is dependent on the total mass of helium in pressure reservoirs as well as the points at which the warm helium intake as well as the cold helium exhaust end....
Directivity of a simplified aeroengine... Although the geometric description of the engine is simplified - in particular, the annular exhaust is not taken into account - it includes some of the main features of a typical aeroengine: subsonic flow, different diameters at the intake and the exhaust ends and the occurence of various flow velocities at the exhaust end to account for the effects of a jet....
Advanced combustion technologies for gas turbine power plants... Turbulent kinetic energy maps of an excited jet with co-flow in a cavity with a partially closed exhaust end are given with and without a longitudinal or a transverse acoustic field....
