1-8 of 8
Keywords: mist cooling
Close
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Heat Mass Transfer. November 2023, 145(11): 113701.
Paper No: HT-22-1780
Published Online: August 11, 2023
... higher mist cooling enhancement of 100% when compared to that of the unconfined scheme at the stagnation point. In terms of total pressure losses, both confined cases have almost the same total pressure losses (see Table 4 ). However, the unconfined case has lower total pressure losses, see Table 4...
Includes: Supplementary data
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Heat Mass Transfer. January 2012, 134(1): 011501.
Published Online: October 28, 2011
... that the droplet-wall interaction is stronger on the pressure side than on the suction side, resulting in a higher mist cooling enhancement on the pressure side. The average rates of mist cooling enhancement of about 15% and 35% were achieved under laboratory and elevated conditions, respectively. This translates...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Heat Mass Transfer. December 2010, 132(12): 122201.
Published Online: September 17, 2010
... of staggered impinging jets. The calibrated CFD model was then used to predict the mist cooling enhancement at the elevated gas turbine working condition. Using the experimental results, the CFD model has been tuned by employing different turbulence models, computational cells, and wall y + values. In addition...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Heat Mass Transfer. December 2008, 130(12): 121901.
Published Online: September 15, 2008
.... The film cooling coverage could switch from the suction side to the pressure side and leave the surface of the other part unprotected by the cooling film. Under real gas turbine operating conditions at high temperature, pressure, and velocity, mist-cooling enhancement could reach up to 20% and provide...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Heat Mass Transfer. October 2008, 130(10): 102901.
Published Online: August 8, 2008
... has the prolonged effect of cooling the region downstream for 15 jet hole diameters, where conventional air film cooling is not effective. 10 07 2007 28 11 2007 08 08 2008 blades cooling flow simulation gas turbines nozzles two-phase flow film cooling mist cooling...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Heat Mass Transfer. April 2007, 129(4): 472–482.
Published Online: January 3, 2007
... cooling mist cooling two-phase flow simulation For more than half a century ( 1 2 ), air film cooling has been commonly applied to cool gas turbine hot components such as combustor liners, combustor transition pieces, turbine vanes (nozzles), and blades (buckets). Numerous studies have been...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Heat Mass Transfer. June 2006, 128(6): 509–519.
Published Online: December 9, 2005
... 12 2005 cooling film flow flow simulation coolants drops diffusion jets film cooling turbine-blade cooling mist cooling Cooling of gas turbine hot-section components, such as combustor liners, combustor transition pieces, turbine vanes (nozzles) and blades (buckets), has...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Heat Mass Transfer. June 2003, 125(3): 438–446.
Published Online: May 20, 2003
... 20 05 2003 disperse systems steam heat transfer drops cooling flow simulation external flows Mist Cooling Enhanced Heat Transfer Impingment Jets Wachters et al. 5 considered the impact of droplets about 60 μm onto a heated surface at velocities in the range of 5 m/s...