The heat/mass transfer analogy for a simulated turbine blade
type: Item
instance of: scholarly article
title: The heat/mass transfer analogy for a simulated turbine blade
zbMATH Open document ID: 1154.80322
author: B. E. Eshmatov
published in: International Journal of Heat and Mass Transfer
publication date: 2008-11-20T00:00:00Z
Mathematics Subject Classification ID: 80A20
Mathematics Subject Classification ID: 80-05
zbMATH DE Number: 5369366
zbMATH Keywords: the heat/mass transfer analogy
zbMATH Keywords: naphthalene sublimation
zbMATH Keywords: thermal boundary layer
zbMATH Keywords: constant temperature
zbMATH Keywords: constant concentration
zbMATH Keywords: gas turbine
zbMATH Keywords: turbine blade
MaRDI profile type: Publication
full work available at URL: j.ijheatmasstransfer.2008.04.002
OpenAlex ID: W2090415669
cites work: The heat/mass transfer analogy factor Nu/Sh, for boundary layers on turbine blade profiles.
cites work: The heat/mass transfer analogy for a simulated turbine endwall
cites work: Q5660738
DOI: 10.1016/J.IJHEATMASSTRANSFER.2008.04.002
Recommended article: The heat/mass transfer analogy for a simulated turbine endwall
Recommended article: Heat transfer on a film-cooled rotating blade using different turbulence models
Recommended article: Numerical simulation of turbine cascade flow with blade-fluid heat exchange
Recommended article: Numerical simulation of steady-state heat transfer in a ceramic-coated gas turbine blade
Recommended article: Q4368435
Recommended article: The heat/mass transfer analogy factor Nu/Sh, for boundary layers on turbine blade profiles.
Recommended article: Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model
Recommended article: Q4652239
Recommended article: Modelling of convective heat and mass transfer in rotating flows
description: scientific article; zbMATH DE number 5369366