Effect of the Radial Pressure Gradient on the Secondary Flow Generated in an Annular Turbine Cascade

TEKRIWAL, P. (1995). Prediction of Heat Transfer For Turbulent Flow in Rotating Radial Duct. International Journal of Rotating Machinery, 1995(), f51-58. https://doi.org/10.1155/S1023621X95000200
Michelassi, V., & G.Wissink, J. (2015). Turbulent Kinetic Energy Production in the Vane of a Low-Pressure Linear Turbine Cascade with Incoming Wakes. International Journal of Rotating Machinery, 2015(), 4-18. https://doi.org/10.1155/2015/650783
Tai, C. H., Wang, D. S., Chen, P. H., Hsu, U. K., & Miao, J. M. (2001). Numerical Studies of the Passage Flowfield in a 3-D Transonic Turbine Blade Cascade. The Chinese Journal of Mechanics, 17(4), 221-230. https://www.airitilibrary.com/Article/Detail?DocID=16800893-200112-17-4-221-230-a
Batsh, H. M. E., Nada, S. A., Abdo, S. N., & Tayesh, A. A. E. (2013). Effect of Secondary Flows on Heat Transfer of a Gas Turbine Blade. International Journal of Rotating Machinery, 2013(), 179-190. https://doi.org/10.1155/2013/797841
TORII, S., & YANG, W. J. (2002). Numerical Analysis on Flow and Heat Transfer in an Axially Rotating Flow Passage with a Concentric Orifice. International Journal of Rotating Machinery, 2002(), 305-308. https://doi.org/10.1155/S1023621X02000283