Investigations on an experimental air-cooled turbine
The effects of cooling on the overall turbine aerodynamic performance and initial operation at an inlet gas temperature of 1400 deg K / by D. E. Fray and N. E. Waldren
1960
53 S.
3/4
Miscellaneous
English
RVK: | ZO 7000 |
Investigations on an experimental air-cooled turbine
SLUB | 1957
|AIAA-2007-1297 EXPERIMENTAL AND CFD INVESTIGATIONS OF FLOW IN COOLED AXIAL HIGH PRESSURE TURBINE
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|An Experimental Single-stage Air-cooled Turbine
Emerald Group Publishing | 1953
|An Experimental Single-stage Air-cooled Turbine
Emerald Group Publishing | 1953
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