Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Boris Glezer"'
Publikováno v:
Journal of Turbomachinery. 124:251-259
Experimental heat transfer results are presented in a two-pass rectangular channel (aspect ratio=2:1) with smooth and ribbed surfaces for two channel orientations (90 and 135 deg to the direction of rotational plane). The rib turbulators are placed o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba645dadaf9a4452b7155ecc3dee89ba
https://doi.org/10.1115/1.1450569
https://doi.org/10.1115/1.1450569
Publikováno v:
Journal of Turbomachinery. 123:697-703
The current paper deals with the aerodynamic measurements in the rotational frame of reference of the Axial Flow Turbine Research Facility (AFTRF) at the Pennsylvania State University. Stationary frame measurements of “Mainstream Aerodynamic Effect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4db1ffa8c878314329a43aba9f9fbcad
https://doi.org/10.1115/1.1397303
https://doi.org/10.1115/1.1397303
Publikováno v:
Journal of Turbomachinery. 123:687-696
The current paper deals with the aerodynamic measurements in the rotational frame of reference of the Axial Flow Turbine Research Facility (AFTRF) at the Pennsylvania State University. Stationary frame measurements of ‘‘Mainstream Aerodynamic Eff
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fbd92d161d8fd8d0b6e564780edc1f0a
https://doi.org/10.1115/1.1401026
https://doi.org/10.1115/1.1401026
Publikováno v:
Journal of Turbomachinery. 123:238-248
The internal fluid mechanics losses generated between the blade plenum chamber and a reference point located just downstream of the trailing edge are investigated for a turbine blade trailing edge cooling system. The discharge coefficient Cd is prese
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c58750c55147c344bd73d3276a4445c3
https://doi.org/10.1115/1.1348017
https://doi.org/10.1115/1.1348017
Publikováno v:
International Journal of Heat and Mass Transfer. 42:4081-4091
Nusselt numbers are presented for a swirl chamber with multiple inlets and helical flow for Reynolds numbers from 6100 to 19,200, and ratios of inlet temperature to wall temperature from 0.60 to 0.95. Local Nusselt numbers, measured over the entire i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fefb07b93216675ba7b1a039027eed99
https://doi.org/10.1016/s0017-9310(99)00086-1
https://doi.org/10.1016/s0017-9310(99)00086-1
Publikováno v:
Experiments in Fluids. 26:347-357
Results are presented from a swirl chamber with and without controlled inlet forcing. The controlled inlet forcing is induced using arrays of vortex generators placed along one wall of the swirl chamber inlet duct. Flow visualization results are give
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fd003dac6312e554d2858b72929f538
https://doi.org/10.1007/s003480050298
https://doi.org/10.1007/s003480050298
Autor:
Boris Glezer, Cengiz Camci
Publikováno v:
Journal of Heat Transfer. 119:20-29
Liquid crystal thermography is an effective method widely employed in transient and steady-state heat transfer experiments with excellent spatial resolution and good accuracy. Most of the past studies in liquid crystal thermography deal with stationa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d89c6df78fb1e2d94ece6042b9f15299
https://doi.org/10.1115/1.2824095
https://doi.org/10.1115/1.2824095
Autor:
Boris Glezer
Publikováno v:
Handbook of Turbomachinery ISBN: 9780824709952
Handbook of Turbomachinery
Handbook of Turbomachinery
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::93f8c8e5722cf82cdfd2cf713fef816a
https://doi.org/10.1201/9780203911990.ch4
https://doi.org/10.1201/9780203911990.ch4
Autor:
Boris Glezer
Publikováno v:
Annals of the New York Academy of Sciences. 934
The presented paper describes a multi-disciplinary cooling selection approach applied to major gas turbine engine hot section components, including turbine nozzles, blades, discs, combustors and support structures, which maintain blade tip clearances
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ac9ec8d8abadf12cd3aa843e696df519
https://pubmed.ncbi.nlm.nih.gov/11460630
https://pubmed.ncbi.nlm.nih.gov/11460630
Publikováno v:
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration.
Experimental heat transfer results are presented in a two-pass rectangular channel (aspect ratio=2:1) with smooth and ribbed surfaces for two channel orientations (90° and 135° to the direction of rotational plane). The rib turbulators are placed o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b0354f1552bfe53c000eeb7b03386dad
https://doi.org/10.1115/2001-gt-0186
https://doi.org/10.1115/2001-gt-0186