1. John D. Denton, (2002), The Effects of Lean and Sweep on Transonic Fan Performance: A Computational Study, Task Quarterly, Vol. 6, No. 1, pp. 7–23.
2. Chen Mao-zhang, (2002) Development of Fan/Compressor Techniques and Suggestions on Further Researches, Journal of Aerospace Power, Vol. 17, No. 1.
3. V. -M. Lei, Z. S. Spakovszky, E. M. Greitzer, (2008), A Criterion for Axial Compressor Hub-Corner Stall, ASME paper GT2008-031006, Berlin.
4. Filippov G A, Wang Zhongqi, (1963) The Calculation of Axial Symmetric Flow in a Turbine Stage with Small Ratio of Diameter to Blade Length. Journal of Moscow Power Institute, Vol. 47, pp. 63–78.
5. Zeyan Peng, Gang Liu, Xingmin Gui, et al.,The Principle of Aviation Turbomachinery [M], Beijing: National Defence Industry Press, 2009.