[1] Wennerstrom AJ (1989) Low aspect ratio axial flow compressor: Why and what it means. J Turbomach 111(4): 357-364.
[2] Cunnan WS, Stevans W, Urasek DC (1978) Design and performance of a 427-meter-per-second-tip-speed two stage fan having a 2.40 pressure ratio. NASA Technical Paper 1314.
[3] Urasek DC, William TG, Cunnan WS (1979) Performance Of a two stage fan having low aspect ratio first stage rotor blading. NASA Technical Paper 1493.
[4] Lakshminarayana B (1996) Fluid dynamics and heat transfer of turbomachinery. John Wiley & Sons, New York, 1996.
[5] Hirsch C, Denton JD (1981) Throughflow calculations in axial turbomachines. AGARD Advisory report, No. 175، AGARD-AR-175.1981.
[6] Pachidis V (2007) Prediction of engine performance under compressor inlet flow distortion using streamline curvatur. J Eng Gas Turbines Power 129(1): 97-103.
[7] Wu CH (1952) A General through-flow theory of flow in subsonic and supersonic turbomachines of axial-mixed-flow types. NASA Report, No. TN2604.
[8] Hearsey RM (1986) Practical compressor aerodynamic design. advanced topics in turbomachinery technolog. Principal Lecture Series No. 2, Concepts ETI.
[9] Templalexis I, Pilidis P, Pachidis V (2011) Development of a two-dimensional streamline curvature code. J Turbomach 133(1): 1-7.
[10] Hu JF, Ou-Yang H, Zhu X Ch, Qiang XQ, Du Z (2011) An improved streamline curvature approach for transonic axial compressor performance prediction. J Aerospace Eng 225(5): 575-584.
[11] Gong WQ,
Wu RK,
Zhang B (2016) A new finite difference method to solve the velocity gradient equation in streamline curvature method. Adv Mech Eng 8(9): 1-13.
[12] Novak RA (1967) Streamline curvature computing procedures flow problems. J Eng Power-T ASME 89(4): 478-490.
[13] Jansen W, Moffatt WC (1967) The off-design analysis compressors. J Eng Power-T ASME 89(4): 453-462.
[14] Wilkinson DH (1970) Stability, convergence and accuracy of two-dimensional streamline curvature methods using quasi-orthogonals. 2nd edn. Proc Inst Mech Engrs 184: 108-119.
[15] Koch CC, Smith LH (1976) Loss sources and magnitudes in axial flow compressors. J Eng Power-T ASME 98(3): 411-424.
[16] Swan WC (1958) A practical method of predicting transonic-compressor performance. J Eng Power-T ASME 83(3): 322-330.
[17] Griepentrog HR (1960) Secondary flow losses in axial compressors. AGARD LS 39, No. 3136.
[18] Storer JA, Cumpsty NA (1994) An aproximation analysis and predition method for tip clearance loss in axial compressors. J Turbomach 116(4): 648-656.
[19] Boyer KM (2003) An improved streamline curvature approach for off-design analysis of transonic compression systems. J Turbomach 125(3): 475-481.
[20] Urasek DC, William TG, Cunnan WS (1979) Performance of a two stage fan having low aspect ratio first stage rotor blading. NASA Technical Paper, 1493.
[21] Cunnan WS, Stevans W, Urasek DC (1978) Design and performance of a 427-meter-per-second-tip-speed two stage fan having a 2.40 pressure ratio. NASA Technical Paper, 1314.