.... , Setoguchi , T. , and Saruwatari , T. , 1988 , “ Studies on the Wells Turbine for Wave Energy Generation (Turbine Characteristics and Design Parameter for Irregular Wave) ,” JSME Int. J. 0913-185X , 31 , pp. 676 – 682 . blades confined flow pattern formation turbines wave power...

... 10 2010 21 04 2011 21 04 2011 compressible flow compressors confined flow Navier-Stokes equations rotating stall surge fan speed stall hysteresis stall inception stall recovery Recipient of the IGTI Technical Committee Best Paper Award for 2010. Rotating...

... 2011 28 02 2011 aerodynamics confined flow coolants cooling finite element analysis gas turbines heat transfer nozzles painting probes thermal conductivity Film cooling with cylindrical or fan-shaped hole geometries in turbine components is one of the main cooling...

... = p 0 , 2 Hence A12 p 1 + 1 2 ρ U 1 2 = p 2 + 1 2 ρ U 2 2 which is simply Bernoulli’s equation for flow through a stream tube. 23 07 2009 07 08 2009 12 11 2010 12 11 2010 blades compressible flow confined flow gas...

... tools may supply a preliminary quantitative description of all relevant physical phenomena, those set in a wheel space region. computational fluid dynamics confined flow design engineering discs (structures) drag engines flow simulation friction gas turbines heat transfer rotational...

... with the industrial rig test data was observed. It is shown that the coupled solutions can be obtained in sufficiently short turn-around times (typically within a week) for use in design. 26 08 2008 11 02 2009 05 04 2010 05 04 2010 compressors computational fluid dynamics confined flow...

... regime without the rotating stall and surge. As of yet, the origin of such dangerous phenomenon has not been investigated in great detail. blades compressors confined flow failure (mechanical) fatigue flow instability flow simulation gas turbines pulsatile flow rotors stators...

... boundary layer turbulence confined flow shear turbulence wakes Aerofoils of a modern low-pressure turbine (LPT) are subjected to increasingly stronger pressure gradient as designers impose higher loading in an effort to improve efficiency and lower cost by reducing the number of blades...

... competitive with the RSM, whereas its computational cost is significantly less than that of the RSM. 21 08 2008 07 10 2008 02 07 2009 aerospace components confined flow rotational flow turbomachinery turbulence Despite a fast growth of computing power and more and more...

... 08 2007 30 06 2009 blades combustion combustion equipment confined flow engines film condensation gas turbines nozzles temperature distribution film cooling hot streak superposition Modeling of “hot streaks” downstream of the combustor in the turbine section...

... load on the rotor blade. The authors wish to acknowledge the financial support from the National 973 Research Program of China through Grant No. 2007CB210108. 09 04 2008 13 04 2008 20 04 2009 blades confined flow flow instability flow simulation heat transfer numerical...

... for axial gap seals and the experiments showed a reasonable agreement for both close- and wide-spaced stages. 30 03 2007 24 08 2007 22 01 2009 aerospace engines blades cadmium cavitation confined flow cooling discs (structures) flow simulation gas turbines numerical analysis...

... to be understood thoroughly and new opportunities exploited where this is feasible.a 08 06 2007 28 06 2007 22 01 2009 aerospace engines blades bubbles compressors confined flow flow separation gas turbines heat transfer jets laminar to turbulent transitions plates (structures...

... in the turbine design process. In high pressure (HP) steam turbines, shrouded blades are commonly used in order to minimize and control the leakage flow. aerodynamics cavitation confined flow steam turbines 18 06 2007 19 06 2007 17 06 2008 2008 American Society...

... the vortical pattern inside the cavity. 27 06 2006 18 08 2006 29 02 2008 aerodynamics blades computational fluid dynamics confined flow cooling design engineering failure analysis rotors turbines vortices Tip clearance between the blade tip of a rotor and the casing...

... of the cavity flow. 03 06 2006 09 10 2006 28 01 2008 turbines vortices confined flow blades flow visualisation aerodynamics flow separation Shrouds are used to prevent pressure-driven leakage flow across the turbine blade tip. Nevertheless, there is still a gap between...

... design is outlined, and the expectation is established that various future designs will require the integrity of the new model; old models can be used in limited cases with care. 01 10 2004 01 02 2005 28 01 2008 design engineering turbomachinery flow simulation confined flow...

... distances. The latter one is the main topic of the investigation presented in the present paper. heat transfer gas turbines micromechanical devices compressors microfluidics confined flow flow simulation 20 06 2006 11 10 2006 2007 American Society of Mechanical Engineers ...

... elucidated. blades confined flow impellers compressors transonic flow flow visualisation subsonic flow flow instability computational fluid dynamics wakes 23 07 2006 11 08 2006 Figure 2 indicates the meridian configuration and the PIV measurement locations. Diffuser...

... of the design of Pelton turbines. 16 11 2004 09 01 2006 turbines jets flow visualisation two-phase flow flow instability numerical analysis confined flow The bucket geometry is partially provided due to confidentiality. Up to now, Pelton turbines have been designed using...