The heat/mass transfer analogy for a simulated turbine blade
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Publication:955546
DOI10.1016/J.IJHEATMASSTRANSFER.2008.04.002zbMath1154.80322OpenAlexW2090415669MaRDI QIDQ955546
Publication date: 20 November 2008
Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.ijheatmasstransfer.2008.04.002
thermal boundary layerturbine bladeconstant temperaturegas turbineconstant concentrationnaphthalene sublimationthe heat/mass transfer analogy
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