Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model

International Journal of Heat and Mass Transfer

Volumn 45, Issue 4, 2001, Pages 815-829

  Schobeiri, M T ^a   Chakka, P ^a  

^a Texas AandM University   (United States)

Author keywords

Boundary layer transition; Turbine blades; Unsteady

Indexed keywords

AERODYNAMICS; BOUNDARY LAYER FLOW; GAS TURBINES; HEAT TRANSFER; MATHEMATICAL MODELS;

GAS TURBINE BLADES;

TURBOMACHINE BLADES;

AERODYNAMICS; BLADE; BOUNDARY LAYER; HEAT TRANSFER; MATHEMATICAL ANALYSIS; TURBINE; TURBOMACHINERY;

EID: 0035910055     PISSN: 00179310     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0017-9310(01)00190-9     Document Type: Article

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