A high rim speed turbine incorporating 3-D features is designed and tested. The cold flow turbine testing, with performance measurements, rotor exit traversing and surface static pressure measurements on the vane and rotor, is performed. The vane is tested in annular cascade on the isentropic light piston cascade. Surface heat transfer measurements on the vanes and endwalls and aerodynamic information are given. The data is compared with design predictions and the reasons for the differences observed are explored.
Aerodynamic and Heat Transfer Measurements on Blading for a High RIM-Speed Transonic Turbine
1989
11 pages
Report
Keine Angabe
Englisch
Engineering Index Backfile | 1928
|British Library Conference Proceedings | 2009
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