| Download | - View final version: Further pressure loss tests on a flat-bladed turbine nozzle cascade (PDF, 5.2 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40004005 |
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| Author | Search for: Cardy, D.F.1 |
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| Affiliation | - National Research Council Canada. Division of Mechanical Engineering
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| Format | Text, Memorandum |
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| Physical description | 33 p. |
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| Abstract | This memorandum presents the results of further pressure loss tests made on a cold-airs low-pressures rig simulating a segment of a tip turbine stator assembly and supply ducts characterized by flat-plate nozzle blades.
A range of nozzles, involving varying side wall shapes passage section and blade geometry has been tested. The effect of air entry angle has also been briefly investigated. |
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| Date published | 1960-10-24 |
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| Publisher | National Research Council of Canada |
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| Series | |
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| Language | English |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 41dbb139-337a-4714-a3d6-d1abc01a2b15 |
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| Record created | 2026-04-08 |
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| Record modified | 2026-04-21 |
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