| Download | - View final version: CF-105. N.A.E. low speed wind tunnel tests January 1956: longitudinal derivatives and comparison with C.A.L. (PDF, 15.9 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40002333 |
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| Creator | Search for: Avro Aircraft Limited (Canada). Technical Department. Stability and Control Group |
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| Format | Text, Data |
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| Physical description | 1 PDF/A (15 MB), 30 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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| Publication date | 1956-04 |
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| Date distributed online | 2021-06-07 |
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| Publisher | Avro Aircraft Limited (Canada). Technical Department. Stability and Control Group |
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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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| Note | Distributed online by the National Research Council of Canada |
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| Language | English |
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| Identifier | P-Wind Tunnel-108 |
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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 | 5fc371cb-f205-4bd3-8451-0f022ea296a0 |
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| Record created | 2021-06-03 |
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| Record modified | 2021-06-07 |
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