| Download | - View final version: Pressure loss and angle tests on a cambered aerofoil turbine nozzle cascade (PDF, 4.3 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003801 |
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| Author | Search for: Smith, B. G.1 |
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| Affiliation | - National Research Council of Canada. Division of Mechanical Engineering
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| Format | Text, Memorandum |
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| Physical description | 22 p. |
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| Abstract | This memorandum describes a series of tests on a conventional gas turbine nozzle blade under conditions similar to those encountered in the N.R.C. Fan-in-Wing scheme.
Total pressure losses and air efflux angles have been measured within a small range of incidence on two designs of blade» The effect of a, constant span, aspect ratio change of one design has also been briefly investigated.
Results have shown that the conventional blade nozzle compared favourably with the "flat-plate" design the total pressure losses being 6.4% and 8.36% respectively. Mean air efflux angles have been found to be within 2½° of the design value under all conditions tested.»» |
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| Publication date | 1961-09 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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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 | 58e79d2a-1c69-4129-b3eb-7f25f5e9fe23 |
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| Record created | 2025-10-24 |
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| Record modified | 2025-11-03 |
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