1. Rolls-Royce, Trent 1000 — the engine walkthrough, lectured in BUAA, March (2006), Beijing.
2. Gui Xingmin, Zhu Fang, Jin Donghai, Aerodynamic Design Report of Tested Scaled Fan, Beijing University of Aeronautics and Astronautics, Beijing, (2012).
3. Beatty, L.A., Savage, M., and Emery, J.C, Low Speed Cascade Tests of Two 45 Degree Swept Compressor Blades With Constant Spanwise Loading, NACA RM L53L07, (1954).
4. Goodwin, W.R., Effect of Sweep on Performance of Compressor Blade Sections as Indicated by Swept Blade Rotor, Unswept Blade Rotor and Cascade Tests. NACA TN 4062, (1957).
5. Smith, L.H. and Yeh, H., Sweep and Dihedral Effect in Axial Flow Turbomachinery. ASME Journal of Basic Engineering, Vol. 85, (1963).