| Download | - View final version: Design, calibration and correction of a 1.6 Mach number nozzle (PDF, 7.8 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003486 |
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| Author | Search for: Laberge, J. G.1 |
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| Affiliation | - National Research Council Canada
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| Format | Text, Technical Report |
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| Physical description | 26 p. |
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| Abstract | The calculation of the theoretical liner profile for M = 1.6, calibration tests and the method of correcting the liner to improve the velocity distribution in the work- ing section of a 10 in. by 10 in, wind tunnel are described, |
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| Publication date | 1952-11-05 |
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| Publisher | National Research Council of Canada. National Aeronautical Establishment |
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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 | 22a054d3-2653-480f-8175-fe162657b1c8 |
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| Record created | 2025-05-09 |
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| Record modified | 2025-05-09 |
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