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Zhong, F. and Zhou, C.*, “Effects of Tip Gap Size on the Aerodynamic Performance of a Cavity-winglet Tip in a Turbine Cascade,” Journal of Turbomachinery, 2017, Vol. 139 No.10, pp.101009-101009-9.
Release time:2022-12-23
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Pre One:
Cao, Z., Zhou, C*, and Sun, Z., “The comparison of the aerodynamic characteristics between a novel highly loaded injected blade with curvature induced pressure-recovery concept and a conventional design,” Chinese Journal of Aeronautics, 2017, Vol.30 No. 3 pp.939-950.
Next One:
Zhou, C.* and Zhong, F., “A Novel Suction Side Winglet Design Philosophy for High Pressure Turbine Rotor Tips,” J. Turbomach., 2017, Vol. 139 No.11, pp:111002-111002-11.
