| Download | - View final version: Directional stability tests at M=1.57 on a 1/80 scale model of the Avro C-105 aircraft with certain modifications (PDF, 5.7 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40001499 |
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| Creator | Search for: Lukasiewicz, J.; Search for: Van Der Bliek, J. A. |
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| Format | Text, Technical Report |
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| Physical description | 1 PDF/A (5 MB), 24 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 | Factors affecting directional stability are reviewed in relation to the C-105 configuration.
Flow visualization and force tests were carried out at M=1.57 on standard C-105 configuration and on 5 modifications involving ventral fins, wing fins, enlarged vertical tail and wing fences. The results of tests indicated in general favourable effects of four modifications on directional stability.
Comparison with NACA data indicates satisfactory agreement. |
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| Publication date | 1957-05-17 |
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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 | 9e8f4495-d727-4724-88da-c44486c8b247 |
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| Record created | 2021-06-03 |
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| Record modified | 2022-05-19 |
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