507
8. Hah C, Shin H-W (2012) Study of near-stall flow behaviour in modern transonic fan with
compound sweep. J Fluids Eng 134:071101
9. Happel H-W, Stubert B (1988) Application of a 3D time-marching Euler code to transonic
turbomachinery flow. Proceedings 7th GAMM-conference on numerical methods in fluid
dynamics. Vieweg Verlag, ISBN 3-528-08094-9, pp 120–129
10. Lewis RI (1996) Turbomachinery performance analysis. Wiley, New York, ISBN 0-47023596-9
11. Lieblein S (1965) Experimental flow in two-dimensional cascades. Chapter 6 of aerodynamic
design of axial-flow compressors. NASA SP-36
12. Lieblein S, Schwenk FC, Broderick RL (1953) Diffusion factor for estimating losses and
limit blade loadings in axial-flow compressor blade elements. NACA RM E53D01
13. NASA-SP-36 (1965) several authors, aerodynamic design of axial-flow compressors. No
ISBN
14. Rechter H, Steinert W, Lehmann K (1985) Comparison of controlled diffusion airfoils with
conventional NACA 65 airfoils developed for stator blade application in a multistage axial
compressor. J Eng Gas Turbines Power 107:494–498
15. Sieverding F, Ribi B, Casey M, Meyer M (2004) Design of industrial axial compressor blade
sections for optimal range and performance. J Turbomach 126:323–331
16. The Jet Engine (1986) Rolls-Royce, ISBN 0-902121-04-9
17. Tweedt DL, Schreiber HA, Starken H (1988) Experimental investigation of the performance
of a supersonic compressor cascade. J Turbomach 110:456–466
18. Wadia AR, Szucs PN, Crall DW (1998) Inner workings of aerodynamic sweep. J Turbomach
120:671–682
References
8. Hah C, Shin H-W (2012) Study of near-stall flow behaviour in modern transonic fan with
compound sweep. J Fluids Eng 134:071101
9. Happel H-W, Stubert B (1988) Application of a 3D time-marching Euler code to transonic
turbomachinery flow. Proceedings 7th GAMM-conference on numerical methods in fluid
dynamics. Vieweg Verlag, ISBN 3-528-08094-9, pp 120–129
10. Lewis RI (1996) Turbomachinery performance analysis. Wiley, New York, ISBN 0-47023596-9
11. Lieblein S (1965) Experimental flow in two-dimensional cascades. Chapter 6 of aerodynamic
design of axial-flow compressors. NASA SP-36
12. Lieblein S, Schwenk FC, Broderick RL (1953) Diffusion factor for estimating losses and
limit blade loadings in axial-flow compressor blade elements. NACA RM E53D01
13. NASA-SP-36 (1965) several authors, aerodynamic design of axial-flow compressors. No
ISBN
14. Rechter H, Steinert W, Lehmann K (1985) Comparison of controlled diffusion airfoils with
conventional NACA 65 airfoils developed for stator blade application in a multistage axial
compressor. J Eng Gas Turbines Power 107:494–498
15. Sieverding F, Ribi B, Casey M, Meyer M (2004) Design of industrial axial compressor blade
sections for optimal range and performance. J Turbomach 126:323–331
16. The Jet Engine (1986) Rolls-Royce, ISBN 0-902121-04-9
17. Tweedt DL, Schreiber HA, Starken H (1988) Experimental investigation of the performance
of a supersonic compressor cascade. J Turbomach 110:456–466
18. Wadia AR, Szucs PN, Crall DW (1998) Inner workings of aerodynamic sweep. J Turbomach
120:671–682
References