Measurements in the transition region of a turbine blade profile under compressible conditions
The suction surface of a linear transonic turbine cascade was experimentally investigated. The transition region was measured by utilizing hot film anemometry and the cascade was instrumented with an array of Senflex nickel heated hot film sensors. To determine the boundary layer edge Mach number di...
| Main Authors: | , |
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| Format: | Journal article |
| Language: | English |
| Published: |
2005
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