1. Kofskey MG, Nusbaum WJ (1968) Aerodynamic evaluation of two-stage axial-flow turbine designed for brayton-cycle space power system. Technical note NASA TN D-4382
2. Dring RP, Joslyn HD, Blair MF (1987) The effect of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of large scale rotating turbine model. NASA Report CR 179469
3. Denton JD (1993) Loss mechanisms in turbomachines. ASME Paper, 93-GT-435
4. Ning W (2000) Significance of loss models in aerothermodynamic simulation for axial flow turbines. PhD thesis, RIT, Sweden
5. Subbarao R, Govardhan M (2012) Effect of axial gap on the aerodynamics of a single stage turbine. J Earth Sci Eng 1:371–377