... change in HTC number were lower than 0.1% when compared to the original neutral positioning. 04 05 2011 15 08 2011 07 11 2011 07 11 2011 aerodynamics angular velocity blades brakes braking computational fluid dynamics design engineering discs (structures) heat...

... of the nozzle throat diameter 1 T W ∝ 1 D * Decreasing the nozzle throat diameter from an order of 10 −1 m to 10 −3 m shows T / W ratios 100 times greater than those of conventional rocket engines are possible. boilers cooling design engineering fuel nozzles...

.... , 1949 , “ Proposed Correlation of Data for Isothermal Two-Phase, Two-Component Flow in Pipes ,” Chem. Eng. Prog. , 45 ( 1 ), pp. 39 – 45 . 31 Klein , S. A. , 2009 , Engineering Equation Solver, F-Chart Software . absorption air conditioning design engineering heat exchangers...

... temperature drops, resulting in a high effective thermal conductivity. design engineering heat conduction heat pipes 09 12 2010 07 04 2011 05 07 2011 05 07 2011 2011 American Society of Mechanical Engineers ...

... values than the case using four separate injections. 08 10 2010 18 01 2011 11 04 2011 11 04 2011 coal gasification computational fluid dynamics design engineering drops flow simulation fuel systems jets numerical analysis oxygen slurries stratified flow two-phase...

... are about 13% and 2%, respectively ( 1 ). sponge iron plant heat integration coal consumption economic analysis coal design engineering energy conservation heat recovery industrial plants steel manufacture 16 03 2010 19 01 2011 10 03 2011 10 03 2011 2011...

... parameters are studied, leading to identification of the most effective design for a given application. 25 11 2009 16 06 2010 12 08 2010 12 08 2010 blending compressible flow computational fluid dynamics design engineering forced convection machine components natural...

... into a pool near the nose cone where the condensate would then be circulated through the channels by the system rotation and the radial difference in the free surface of the pool and the outlet of the channels. aerospace components design engineering heat pipes heat transfer jet engines 27...

... possible explanation is that the benefit of the developed jet velocity profile diminishes as jet velocities rise and the air has lesser time to develop prior to exiting. 21 10 2008 28 04 2009 20 08 2009 blades combustion equipment cooling design engineering engines gas turbines...