Study on the behavior of small droplet impinging onto a hot surface [PDF]
, 2011 This paper was presented at the 3rd Micro and Nano Flows Conference (MNF2011), which was held at the Makedonia Palace Hotel, Thessaloniki in Greece.
3rd Micro and Nano Flows Conference (MNF2011) +7 more
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Flow visualization study of the effect of injection hole geometry on an inclined jet in crossflow [PDF]
A flow visualization was studied by using neutrally buoyant, helium-filled soap bubbles, to determine the effect of injection hole geometry on the trajectory of an air jet in a crossflow and to investigate the mechanisms involved in jet deflection ...
Ciancone, M. L., Simon, F. F.
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Analysis for predicting adiabatic wall temperatures with single hole coolant injection into a low speed crossflow [PDF]
Assuming the local adiabatic wall temperature equals the local total temperature in a low speed coolant mixing layer, integral conservation equations with and without the boundary layer effects are formulated for the mixing layer downstream of a single ...
Graham, R. W. +2 more
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Curved film cooling admission tube [PDF]
, 1980 Effective film cooling to protect a wall surface from a hot fluid which impinges on or flows along the surface is provided. A film of cooling fluid having increased area is provided by changing the direction of a stream of cooling fluid through an angle ...
Graham, R. W., Papell, S. S.
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Film cooling on a convex wall: Heat transfer and hydrodynamic measurements for full and partial coverage [PDF]
Turbine-blade cooling is an important issue for high-efficiency turbine engines, and discrete-hole injection is widely used as a cooling method. In the present study, detailed measurements were made of the heat transfer and hydrodynamics of a film-cooled
Furuhama, K. +3 more
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SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
Havacılık ve Uzay Teknolojileri Dergisi, 2006 This paper deals with experimental and numerical investigation of the film cooling effectiveness on a flat plate. Eleven injection holes on the model are in a single row. The holes have cylindrical cross section and they are 8.5 mm diameters.
İbrahim Koç
doaj
Small gas turbine combustor study: Combustor liner evaluation [PDF]
For abstract see A83 ...
Norgren, C. T., Riddlebaugh, S. M.
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Flow visualization of discrete hole film cooling for gas turbine applications [PDF]
Film injection from discrete holes in a three row staggered array with 5-diameter spacing is studied. The boundary layer thickness-to-hole diameter ratio and Reynolds number are typical of gas turbine film cooling applications.
Colladay, R. S., Russell, L. M.
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Analysis of metal temperature and coolant flow with a thermal-barrier coating on a full-coverage-film-cooled turbine vane [PDF]
The potential benefits of combining full-coverage film cooling with a thermal-barrier coating were investigated analytically for sections on the suction and pressure sides a high-temperature, high-pressure turbine vane.
Meitner, P. L.
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AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR [PDF]
Gaseous-film cooling of rocket combustion ...
Golladay, R. L., Lucas, J. G.
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