| Download | - View final version: A summary of high speed wind tunnel test results for the Avro CF-105, and their effects on estimated performance (PDF, 13.7 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40001744 |
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| Creator | Search for: Templeton, R. J.; Search for: Michaelsen, O. E. |
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| Format | Text, Technical Report |
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| Physical description | 1 PDF/A (13 MB), 31 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 | This note compares some of the results of model tests on the CF-105, which were carried out in the Cornell transonic tunnel, in the 4 ft. wind tunnels at NACA, Langley, and in the 16 inch x 30 inch high speed tunnel at the NAE. These results are also compared with estimates which were previously made by Avro and NAE of various items which affect performance. |
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| Publication date | 1957 |
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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 | 83ed3d42-4e8d-425a-af07-ae668e2d6909 |
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| Record created | 2021-06-03 |
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| Record modified | 2022-05-19 |
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