1. V. Vassiliev, S. Irmisch, S. Abdel-Wahab, and A. Granovskiy, “Impact of the inflow conditions on the heavy-duty gas turbine exhaust diffuser performance,” J. Turbomach. 134, 041018 (2012).
2. K. M. Popov, M. Kh. Mukhtarov, L. I. Kiselev, and I. V. Safron’ev, “The effect of radial clearance and working blade shrouding on efficiency losses of highloaded cooled turbines,” Tr. Tsentr. Inst. Aviats. Mashinstr., No. 911 (1980).
3. A. M. Wallis, J. D. Denton, and A. A. J. Demargne, “The control of shroud leakage flows to reduce aerodynamic losses in a low aspect ratio, shrouded axial flow turbine,” ASME Paper No. 2000-GT-475 (Am. Soc. Mech. Eng., 2000).
4. L. Porreca, T. Behr, J. Schlienger, A. I. Kalfas, R. S. Abhari, J. Ehrhard, and E. Janke, “Fluid dynamics and performance of partially and fully shrouded axial turbines,” J. Turbomach. 127, 668–678 (2005).
5. K. Wolter, A. Giboni, P. Peters, J. R. Menter, and H. Pfost, “Experimental and numerical investigation of the unsteady leakage flow through the rotor tip labyrinth of a 1.5-stage axial turbine,” ASME Paper No. GT2005-68156 (Am. Soc. Mech. Eng., 2005).