Zobrazeno 1 - 4
of 4
pro vyhledávání: '"D. R. Thurman"'
Publikováno v:
Journal of Turbomachinery. 120:305-313
Turbine blade endwall heat transfer measurements are given for a range of Reynolds and Mach numbers. Data were obtained for Reynolds numbers based on inlet conditions of 0.5 and 1.0 x 106, for isentropic exit Mach numbers of 1.0 and 1.3, and for free
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::07bf1dd3fba6bf15361a2adff69aa983
https://doi.org/10.1115/1.2841407
https://doi.org/10.1115/1.2841407
Publikováno v:
Journal of Flow Visualization and Image Processing. 2:267-283
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a6378a18078b2fa7719029e9dc77b38
https://doi.org/10.1615/jflowvisimageproc.v2.i3.70
https://doi.org/10.1615/jflowvisimageproc.v2.i3.70
Publikováno v:
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration.
Detailed heat transfer measurementa and predictions are given for a turbine rotor with 136° of turning and an axial chord of 12.7 cm. Data were obtained for inlet Reynolds numbers of 0.5 and 1.0 × 106, for isentropic exit Mach numbers of 1.0 and 1.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30681a7625d3fdb2fe566d0ece31bdb1
https://doi.org/10.1115/99-gt-125
https://doi.org/10.1115/99-gt-125
Autor:
I. Lopez, W. P. Camperchioli, P. W. Giel, T. A. Jett, G. J. Van Fossen, R. J. Boyle, D. R. Thurman, H. La
Publikováno v:
Volume 1: Turbomachinery.
Three-dimensional flow field measurements are presented for a large scale transonic turbine blade cascade. Flow field total pressures and pitch and yaw flow angles were measured at an inlet Reynolds number of 1.0 × 106 and at an isentropic exit Mach
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::68a76c7ed35c4b4dd3f254cbd20d9292
https://doi.org/10.1115/96-gt-113
https://doi.org/10.1115/96-gt-113