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The heat/mass transfer analogy factor Nu/Sh, for boundary layers on turbine blade profiles.

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Publication:5932366
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DOI10.1016/S0017-9310(00)00175-7zbMath1058.80505OpenAlexW2010536118MaRDI QIDQ5932366

No author found.

Publication date: 2001

Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0017-9310(00)00175-7



Mathematics Subject Classification ID

Turbulent boundary layers (76F40)


Related Items (3)

The heat/mass transfer analogy for a simulated turbine endwall ⋮ The heat/mass transfer analogy for a simulated turbine blade ⋮ Polar differentiation matrices for the Laplace equation in the disk under nonhomogeneous Dirichlet, Neumann and Robin boundary conditions and the biharmonic equation under nonhomogeneous Dirichlet conditions







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