1 |
Wintucky, W.T., Stewart, W.L., 1957, "Analysis of two-stage counter-rotating turbine efficiencies in terms of work and speed requirements," NACA RM E57L05.
|
2 |
Ozgur, C., Nathan, G.K., 1971, "Study of contra-rotating turbines based on design efficiency," Journal of Basic Engineering, Vol. 93, pp. 395-404.
DOI
|
3 |
Louis, J.F., 1985, "Axial flow contra-rotating turbines", ASME paper, 85-GT-218.
|
4 |
Ji, L.C., Quan, X.B., Wel, L., Xu, J.Z., 2001, "A Vaneless Counter rotating turbine design towards limit of specific work ratio," ISABE paper, 2001-1062.
|
5 |
Zhao, Q.H., Du, J., Wang, H.S., Zhao, X.L., Xu, J.Z., 2010, "Tip clearance effects on inlet hot streak migration characteristics in high pressure stage of a vaneless counter-rotating turbine," Journal of Turbomachinery, Vol. 132, No. 011005, pp. 1-8.
|
6 |
Venable, B.L., Delaney, R.A., Busby, J.A., Davis, R.L., Dorney, D.J., Dunn, M.G., Haldeman, C.W., Abhari, R.S., 1999, "Influence of vane-blade spacing on transonic turbine stage aerodynamics. Part I - time-averaged data and analysis," Journal of Turbomachinery, Vol. 121, pp. 663-672.
DOI
|
7 |
Yamada, K., Funazaki, K., Kikuchi, M., Sato, H., 2009, "Influences of axial gap between blade rows on secondary flows and aerodynamic performance in a turbine stage," GT 2009-59855.
|
8 |
Jeong, E., Park, P.K., Kang, S.H., Kim, J., 2006, "Effect of nozzle-rotor clearance on turbine performance," ASME paper, FEDSM 2006-98388.
|
9 |
Gaetani, P., Persico, G., Dossena, V., Osnaghi, C., 2006, "Investigation of the flow field in a hp turbine stage for two statorrotor axial gaps, Part I-3D time-averaged flow field," GT 2006-90553.
|
10 |
Kikuchi, M., Funazaki, K., Yamada, K., Sato, H., 2008, "Detailed studies on aerodynamic performance and unsteady flow behaviors of a single turbine stage with variable rotor-Stator axial gap," International Journal of Gas Turbine, Propulsion and Power Systems, Vol. 2, No. 1, pp. 30-37.
|
11 |
Sadovnichiy, V.N., Binner, M., Seume, J.R., 2009, "The influence of axial gaps and leaned-twisted guide vanes on the shroud leakage and turbine stage efficiency," Proceedings of the 8th European Conference on Turbomachinery, Austria.
|
12 |
Dring, R.P., Joslyn, H.D., Blair, M.F., 1987, "The effect of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of large scale rotating turbine model," NASA CR-179469.
|
13 |
Caspar J.R., Hobbs., D.E., Davis, R,L., 1980, "Calculation of two-dimensional potential cascade flow using finite area methods," AIAA Journal, Vol. 18, pp. 103-109.
DOI
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