[1] R.N. Sharma, “Economics of mine ventilation,” In Proceedings of International Conference on Mineral Industry: Issues on Economics, Environment and Technology (pp. 75–87). India: The Mining, Geological and Metallurgical Institute of India, (2002).
[2] B. Eck, Fans; “design and operation of centrifugal, axial flow,” and cross-flow fans, Oxford: Pergamon Press, (1973).
[3] P.K. Sen, “Reducing power consumption for axial flow mine ventilation fans,” Journal of Mines, Metals and Fuels, Vol.45, No. (9–10), pp. 301–303, (1997).
[4] W.A. Hustrulid & R.L. Bullock, “Underground mining methods: engineering fundamentals and international case studies,” Englewood, CO: Society for Mining, Metallurgy and Exploration, (2001).
[5] J. Herricl, E. ameesm, and E. Johnr, “Systematic Two-Dimensional Cascade Tests of NACA 65-Series Compressor Blades at Low Speeds,” NACA-TR-1368, (1951).
[6] I. Felixr, “Summary of 65-Series Compressor-Blade Low-Speed Cascade Data by Use of the Carpet-Plotting Technique, NACA-TN-3913, (1954).
[7] Mellorg, “Aerodynamic Performance of Axial Compressor Cascades with Application to Machine Design,” MIT Gas Turbine Lab, Report No. 3S, (1957).
[8] B. Lakshminarayana, “Fluid Dynamics and Heat Transfer of Turbomachinery,” John Wiley & Sons, New York, (1996).
[9] V. Pachidis, “Prediction of engine Performance under Compressor inlet Flow Distortion Using Streamline Curvature,” J. Eng. Power, Vol. 89, No. 4, pp. 478-490, (2006).
[10] Hearsey، R. M, “Practical Compressor Aerodynamic Design, Advanced Topics in Turbomachinery Technolog,” Principal Lecture Series No. 2, Concepts ETI, 1986.
[11] I. Templalexis, P. Pilidis, V. Pachidis, and P. Kotsiopoulos, “ Development of a Two-Dimensional Streamline Curvature Code,” J. Turbomach, Vol. 133, No. 1, 0110031-7, (2011).
[12] J. F. Hu, H. Ou-Yang, X. Ch. ZHu, X. Q. Qiang, and Z. Du, “An improved streamline curvature approach for transonic axial compressor performance prediction,” J. Aerospace Engineering Vol. 225, No. 5, 575-584, (2011).
[13] W. Gong, R. Kang, W. Bin Zhang, “A new finite difference method to solve the velocity gradient equation in streamline curvature method,” Advances in Mechanical Engineering, Vol. 8, No. 9, pp. 1–13, (2016).
[14] C.C. Koch, L. H. Smith, “Loss Sources and Magnitudes in Axial Flow Compressors,” Transactions of the ASME, Journal of Engineering for Power, Vol. 98, No. 3, pp. 411-424, (1976).
[15] W. C. Swan, “A Practical Method Of Predicting Transonic-Compressor Performance,” Journal of Engineering for Power, Vol. 83, No. 3, pp. 322–330, (1958).
[16] H. R. Griepentrog, “Secondary Flow Losses in Axial Compressors,” AGARD LS 39, (1970).
[17] JA Storer and NA cumpsty, “An approximation analysis and prediction method for tip clearance loss in axial compressors,” J. Turbomach, Vol. 116, NO. 4, pp. 648-656, (1994).
[18] S. Lieblein, “Incidence and Deviation-Angle Correlations for Compressor Cascades,” J. Basic Eng Vol. 82, No. 3, pp. 575-584, (1960).
[19] NA. Cumpsty, “Compressor aerodynamics,” John Wiley & Sons. New York, (1989).
[20] D. C. Urasek, T. G. William, W. S. Cunnan, “ Performance Of a Two Stage Fan Having Low Aspect Ratio First Stage Rotor Blading,” NASA Technical Paper 1493, (1979).
[21] G. R. Frost, R. M. Hearsey, A. J. Wennerstrom, “a computer program for the specification of axial compressor airfoils,” project 7065, Aerospace Research Laboratories, (1972).
[22] I.H. Abbott, A.E. Von Doenhoff, “Theory of Wing Sections: Including a Summary of Airfoil Data,” (1959).
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