Zobrazeno 1 - 3
of 3
pro vyhledávání: '"W. P. Camperchioli"'
Publikováno v:
Journal of Turbomachinery. 123:168-177
Turbine vane heat transfer distributions obtained using an infrared camera technique are described. Infrared thermography was used because noncontact surface temperature measurements were desired. Surface temperatures were 80°C or less. Tests were c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::793c8e3613d804e79f3c2410e9e9e900
https://doi.org/10.1115/1.1333693
https://doi.org/10.1115/1.1333693
Publikováno v:
Volume 1: Turbomachinery.
Midspan aerodynamic measurements for a three vane-four passage linear turbine vane cascade are given. The vane axial chord was 4.45cm. Surface pressures and loss coefficients were measured at exit Mach numbers of 0.3, 0.7, and 0.9. Reynolds number wa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91f2aa57aa511cd235e04aa95370666b
https://doi.org/10.1115/98-gt-285
https://doi.org/10.1115/98-gt-285
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