Aero-thermal study of the unsteady flow field in a transonic gas turbine with inlet temperature distortions

CFD prediction of the unsteady aero-thermal interaction in the HP turbine stage, with inlet temperature non-uniformity, requires appropriate unsteady modelling and a low diffusive numerical scheme coupled with suitable turbulence models. This maybe referred to as high fidelity CFD. A numerical study...

詳細記述

書誌詳細
主要な著者: Martelli, F, Adami, P, Salvadori, S, Chana, K, Castillon, L
フォーマット: Journal article
言語:English
出版事項: 2008