An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines

DOI10.1080/17415970500354235zbMath1194.76098OpenAlexW2025789108MaRDI QIDQ3588278

Wahid Ghaly, Kasra Daneshkhah

Publication date: 10 September 2010

Published in: Inverse Problems in Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/17415970500354235

zbMATH Keywords

moving meshReynolds-averaged Navier-StokesALE formulationaerodynamic shape designinverse blade design

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (1)

An inverse design method for viscous flow in turbomachinery blading using a wall virtual movement

Cites Work

• Space conservation law in finite volume calculations of fluid flow

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