[1] Giampaolo A (2006) Gas Turbine Handbook: Principles and Practices. 3nd edn. The Fairmont Press.
[2] Yun Y, Park Y, Song SJ (2005) Performance Degradation Due to Blade Surface Roughness in a Single-Stage Axial Turbine. ASME J Turbomach. 137-143.
[3] Bammert K, Sandstede H (1972) Measurements Concerning the Influence of Surface Roughness and Profile Changes on the Performance of Gas. ASME J Engineering for Power. 207-213.
[4] Kind RJ, Serjac PJ, Abbott MWP (1998) Measurements and Prediction of the Effects of Surface Roughness on Profile Losses and Deviation in a Turbine. ASME J Turbomach. 20-27.
[5] Morini M, Pinelli M, Spina PR, Venturini M (2009) CFD Simulation of Fouling on Axial Compressor Stages. ASME TURBO EXPO.
[6] Morini M, Pinelli M, Spina PR, Venturini M (2010) Numerical Analysis of the Effects of Non-Uniform Surface Roughness on Compressor Stage Performane. ASME TURBO EXPO.
[7] Morini M, Pinelli M, Spina PR, Venturini M (2010) Influence of Blade Deterioration on Compressor and Turbine. ASME J Engineering for Gas Turbines and Power.
[8] Kang YS, Yoo JC, Kang SH (2006) Numerical Predictions of Roughness Effects on the Performance Degradation of an Axial-Turbine Stage. KSME J Mechanical Science and Technology. 1077-1088.
[9] Boyle RJ, Senyitko RG (2003) Measurements and Predictions of Surface Roughness Effects on Turbine Vane Aerodynamics. ASME TURBO EXPO.
[10] Hoffmann AK, Chiang ST (2000) Computational Fluid Dynamics. Vol 1-2-3, 4nd edn, Engineering Education System Publication, USA.
[11] Kermani MJ, Plett E.G (2001) Roe Scheme in Generalized Coordinate. part I- Formulations. AIAA J.
[12] Kermani MJ, Plett E.G (2001) Roe Scheme in Generalized Coordinates, part II- Application to Inviscid and viscous flows. AIAA J.
[13] Blazek J (2001) Computational Fluid Dynamics: Principles and Applications. Elsevier Science Ltd, UK.
[14] Kermani MJ, Plett E.G (2001) Modified Entropy Correction Formula for the Roe Scheme Roe. AIAA J.
[15] Visbal M, Knight D (1984) the Baldwin-Lomax Turbulence Model for Tow-Dimensional Shock-Wave/Boundary Layer Interactions. AIAA J. 921-921.
[16] Shin J, Chen HH, Cebeci T (1992) A Turbulence Model for Iced Airfoils and Its Vaidation. AIAA 30th Aerospace Sciences Meeting.
[17] Back SC, Sohn JH, Song SJ (2010) Impact of Surface Roughness on Compressor Cascade Performance. ASME J Fluids Engineering.
[18] Schlichting H (1979) Boundary Layer Theory. McGraw-Hill Ins. 7th edn, New York.
[19] Lakshminarayana B (1996) Fluid Dynamics and Heat Transfer of Turbomachinery Wiley Interscience Publication, USA.
[20] Dahlquist AN (2008) Investigation of losses prediction methods in 1D for axial gas turbines. MSc thesis. Faculty of Engineering LTH Lund University. Sweden.
[21] Kang SH, Kang YS, Han KH (2003) Numerical Study on Blade Roughness Effect on the Performance of Turbomachines. IGTC.
[22] Guo J, Julien PY (2007) Buffer Law and Transient Roughness Effect in Turbulent Open-Channe. ISEH.