| Download | - View final version: Pressure loss tests on a flat-bladed turbine nozzle cascade (PDF, 4.8 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003998 |
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| Author | Search for: Bassett, R.W.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 | 23 p. |
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| Abstract | This Memorandum presents the results of pressure loss tests made to date on a cold-air, low-pressure, rig simulating a segment of a tip turbine stator assembly and supply duct, and characterized by flat-plate nozzle blades.
A range of pitch/chord ratios has been tested, and the effects on performance of the nozzle shape and blade trailing edge thickness have been briefly investigated. |
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| Publication date | 1960-07-07 |
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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 | aef72cb0-5f61-4562-b116-145b043aeb10 |
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| Record created | 2026-04-08 |
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| Record modified | 2026-04-08 |
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