| Download | - View final version: Six-component super-sonic wind tunnel tests of a 1/80 scale model of the C-105 aircraft (PDF, 253.3 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40001784 |
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| Creator | Search for: Laberge, J. G. |
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| Format | Text, Technical Report |
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| Physical description | 1 PDF/A (253 MB), 310 p. |
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| Subject | Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor |
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| Abstract | Six-component supersonic wind tunnel tests were carried out on a 1/80 scale model of the C-105 aircraft at four Mach numbers. In all, 27 model configurations were investigated over a period of three months requiring a total of 1991 tunnel runs. This memorandum contains the results of these tests in the form of basic plots, cross plots and final aerodynamic derivatives. In order to expedite the publication of the data, the results are presented without detailed analysis. |
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| Publication date | 1956 |
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| Date distributed online | 2021-06-07 |
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| Publisher | National Research Council of Canada. National Aeronautical Establishment. Aerodynamics |
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| Licence | |
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| Access condition | - The print copies are housed in the Rare books collection at the National Research Council of Canada. For access to print, permission to reproduce for commercial purposes, or questions related to the collection please contact NRC.NSL-BSN.CNRC@nrc-cnrc.gc.ca.
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| Series | |
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| Note | Distributed online by the National Research Council of Canada |
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| Language | English |
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| Export citation | Export as RIS |
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| Collection | Avro Canada CF-105 Arrow |
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| Record identifier | e892aff3-5a86-40fb-a4f5-7ce37f5a0e2c |
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| Record created | 2021-06-03 |
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| Record modified | 2022-05-19 |
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