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...

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Detaylı Bibliyografya
Asıl Yazarlar: Martelli, F, Adami, P, Salvadori, S, Chana, K, Castillon, L
Materyal Türü: Journal article
Dil:English
Baskı/Yayın Bilgisi: 2008