Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Shantanu Mhetras"'
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
Ribs were added into a pin fin array for a uniquely new cooling concept enabled through additive manufacturing. Heat transfer measurements are obtained using the thermochromic liquid crystal technique in a trapezoidal duct with pin fins and rib turbu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::194b192b91cba1c71b3c0354d496dd4a
https://doi.org/10.1115/1.4051766
https://doi.org/10.1115/1.4051766
Publikováno v:
Volume 5A: Heat Transfer.
Increasing the firing temperatures in gas turbines require better, and highly efficient means of heat removal of turbine blades so that metal temperatures stay within the limit of safe operation with respect to metal properties. This study focuses on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::da11bf5b27fa544dd3bf4195b74857f1
https://doi.org/10.1115/gt2017-63044
https://doi.org/10.1115/gt2017-63044
Publikováno v:
Journal of Thermophysics and Heat Transfer. 26:75-84
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43d65527d6488adbec274aff71a83de8
https://doi.org/10.2514/1.42411
https://doi.org/10.2514/1.42411
Publikováno v:
Journal of Thermophysics and Heat Transfer. 22:50-61
[Abstract] The film cooling effectiveness on a fully film cooled high pressure turbine blade is investigated using the Pressure Sensitive Paint technique. Three rows of radial angled cylindrical holes are arranged in the leading edge region, while ax
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d89dd30a271cdc048c5dbff02a962060
https://doi.org/10.2514/1.31206
https://doi.org/10.2514/1.31206
Publikováno v:
Journal of Heat Transfer. 127:521-530
Effects of the presence of squealer, the locations of the film-cooling holes, and the tip-gap clearance on the film-cooling effectiveness were studied and compared to those for a plane (flat) tip. The film-cooling effectiveness distributions were mea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79fea7e630a76b6be1922c8f511e31f5
https://doi.org/10.1115/1.1909208
https://doi.org/10.1115/1.1909208
Publikováno v:
Volume 5B: Heat Transfer.
Film-cooling and heat transfer characteristics of a gas turbine blade tip with a suction side rail was investigated in a stationary 3-blade rectilinear cascade. Mounted at the end of a blow-down facility the cascade operated at inlet and exit Mach nu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e19930f258f81c93d706554fdfa2de50
https://doi.org/10.1115/gt2014-25793
https://doi.org/10.1115/gt2014-25793
Publikováno v:
Volume 3A: Heat Transfer.
Experiments to investigate heat transfer and pressure loss are performed in a rectangular channel with an aspect ratio of 6 at very high Reynolds numbers under compressible flow conditions. Reynolds numbers up to 1.3 × 106 are tested. The presence o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0f4938674b5b4f22c144a728bd4b2ccc
https://doi.org/10.1115/gt2013-95891
https://doi.org/10.1115/gt2013-95891
Publikováno v:
Volume 3A: Heat Transfer.
Experiments to investigate heat transfer and pressure loss from jet array impingement are performed on the target wall at high Reynolds numbers. Reynolds numbers up to 450,000 are tested. The presence of a turbulated target wall and its effect on hea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9344c5a24c4a4d1210025ab9189b553e
https://doi.org/10.1115/gt2013-95893
https://doi.org/10.1115/gt2013-95893
Publikováno v:
Journal of Turbomachinery. 134
The effect of film-cooling holes placed along the span of a fully cooled high pressure turbine blade in a stationary, linear cascade on film-cooling effectiveness is studied using the pressure sensitive paint technique. The effect of showerhead injec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7ea2342568da67e6070733744a24205e
https://doi.org/10.1115/1.4003228
https://doi.org/10.1115/1.4003228
Publikováno v:
Journal of Turbomachinery. 131
Film cooling effectiveness measurements under rotation were performed on the rotor blade platform using a pressure sensitive paint (PSP) technique. The present study examines, in particular, the film cooling effectiveness due to purging of coolant fr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e8276815bf92b195623160daa09b53c1
https://doi.org/10.1115/1.2752184
https://doi.org/10.1115/1.2752184