Author:
Wang Jiayu,Hu Jun,Jiang Chao,Li Jun
Publisher
Springer Science and Business Media LLC
Reference37 articles.
1. Lieblein S. Analysis of experimental low-speed loss and stall characteristics of two-dimensional compressor blade cascades. NASA Research Memorandum, paper NACA-RM-E57A28, 1957.
2. Herrig L.J., Emery J.C., Erwin J.R., Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds. Langley Aeronautical Laboratory, 1957.
3. Hausmann G.F., The theoretical induced deflection angle in cascades having wall boundary layers. Journal of the Aeronautical Sciences, 1948, 15(11): 686–690.
4. Lieblein S., Incidence and deviation-angle correlations for compressor cascades. Journal of Basic Engineering, 1960, 82(3): 575–584.
5. Hobbs D.E., Weingold H.D., Development of controlled diffusion airfoils for multistage compressor application. Journal of Engineering for Gas Turbines and Power, 1984, 106(2): 271–278.
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献