Abstract
The flow through a turbomachine is generally three-dimensional, viscous, highly unsteady, transitional, turbulent, and compressible. This complex flow is associated with total pressure losses caused by different flow and geometry parameters. To accurately predict the efficiency of a turbomachine, accurate flow calculation is required.
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Schobeiri, M.T. (2018). Losses in Turbine and Compressor Cascades. In: Gas Turbine Design, Components and System Design Integration. Springer, Cham. https://doi.org/10.1007/978-3-319-58378-5_6
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DOI: https://doi.org/10.1007/978-3-319-58378-5_6
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