Zobrazeno 1 - 4
of 4
pro vyhledávání: '"A. T. Lethander"'
Publikováno v:
Volume 2C: Turbomachinery.
The focus of the study presented here was to investigate the interaction between the blade and downstream vane of the stage-and-one-half transonic turbine via CFD analysis and experimental data. A Reynolds-Averaged Navier-Stokes (RANS) flow solver wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::532ee69ddb562aee33a0880432ac7864
https://doi.org/10.1115/gt2015-42416
https://doi.org/10.1115/gt2015-42416
Publikováno v:
Journal of Turbomachinery. 125:203-209
Most turbine inlet flows resulting from the combustor exit are nonuniform in the near-platform region as a result of cooling methods used for the combustor liner. These cooling methods include injection through film-cooling holes and injection throug
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::631b766fb24d68bb30ddb0b2cbfc34f0
https://doi.org/10.1115/1.1561812
https://doi.org/10.1115/1.1561812
Optimizing the Vane-Endwall Junction to Reduce Adiabatic Wall Temperatures in a Turbine Vane Passage
Publikováno v:
Volume 5: Turbo Expo 2003, Parts A and B.
Secondary flows in airfoil passages have become increasingly important in the design of modern gas turbines due to several fundamental trends in gas turbine engine development. Driven to achieve higher engine efficiencies and specific thrust output,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::458ff8a2bdc5596412243ffb3f6edbe6
https://doi.org/10.1115/gt2003-38939
https://doi.org/10.1115/gt2003-38939
Publikováno v:
Volume 3: Turbo Expo 2002, Parts A and B.
Most turbine inlet flows resulting from the combustor exit are non-uniform in the near-platform region as a result of cooling methods used for the combustor liner. These cooling methods include injection through film-cooling holes and injection throu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aade715da8638465d465f1637cdf9971
https://doi.org/10.1115/gt2002-30527
https://doi.org/10.1115/gt2002-30527