Zhong, F, and Zhou, C.*, “Tip Gap Size Effects on Thermal Performance of Cavity-winglet Tips in Transonic Turbine Cascade with Endwall Motion,” 2017, Journal of the Global Power and Propulsion Society, 2017, Vol. 1, pp41-45
发布时间：2022-12-23 点击次数：
- 上一条：Zhong, F., Zhou, C*, Ma, H., and Zhang, Q., “Heat Transfer of Winglet Tips in a Transonic Turbine Cascade,” Journal of Engineering for Gas Turbines and Power, 2017, Vol. 139, pp. 0126051-01260511.
- 下一条：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.
