Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Connor J. Wiese"'
Publikováno v:
Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling.
An increasingly common experimental technique allows measurement of overall effectiveness by matching the Biot number between experimental and engine conditions. The measured overall effectiveness distribution correlates to the actual turbine compone
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4b480726ad484cec8d3b28db14ff6004
https://doi.org/10.1115/gt2022-81510
https://doi.org/10.1115/gt2022-81510
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
In typical film cooling experiments, the adiabatic wall temperature may be determined from surface temperature measurements on a low thermal conductivity model in a low-temperature wind tunnel. In such experiments, it is generally accepted that the a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5882e56e3f0e43e59367e9d08888616
https://doi.org/10.1115/1.4052810
https://doi.org/10.1115/1.4052810
Publikováno v:
Journal of Turbomachinery. 140
Testing new turbine cooling schemes at engine conditions becomes increasingly cost prohibitive as the desired gas-path temperatures increase. As a result, the turbine component is simulated in a laboratory with a large-scale model that is sized and c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cb3bd08cadbad6334616e7b28f49924b
https://doi.org/10.1115/1.4041292
https://doi.org/10.1115/1.4041292
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51fd8b9fa00f12c33545ffeefd93385c
https://doi.org/10.2514/6.2016-0904
https://doi.org/10.2514/6.2016-0904
Autor:
Michael J McClearn, Richard Iii T Guttman, Giovanni Allevato, Connor J. Wiese, Kurt P. Rouser
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Turbine cascade wind tunnels simulate Reynolds number and turbulence for the examination of flow phenomena such as boundary layer separation on the trailing portion of low pressure turbine blades. Axial chord-based Reynolds numbers considered in this
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c8f2d63debde1e0fe3283dc1d9d71728
https://doi.org/10.2514/6.2015-0380
https://doi.org/10.2514/6.2015-0380