The influence of Coriolis forces and streamwise curvature on boundary layers has been introduced into an integral method by adding a correction term to the dissipation factor. This correction term is related to Coriolis forces and streamline curvature in terms of a parameter 13 which was determined using existing experimental data. Theoretical calculations using this value of show good agreement with experimental results for a wide range of curvature and rotation numbers representing realistic conditions for turbomachinery applications.
- International Gas Turbine Institute
Correction for Streamline Curvature and Coriolis Force in a Boundary Layer Integral Method
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Van Den Braembussche, RA, & Zunino, P. "Correction for Streamline Curvature and Coriolis Force in a Boundary Layer Integral Method." Proceedings of the ASME 1981 International Gas Turbine Conference and Products Show. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. Houston, Texas, USA. March 9–12, 1981. V001T03A021. ASME. https://doi.org/10.1115/81-GT-97
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