| Download | - View final version: Wind tunnel investigation of possible rudder flutter on a 1:25 scale fin model of CF-105 at Mach number of 1.22 (PDF, 2.4 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40001729 |
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| Creator | Search for: Orlik-Ruckemann, K. |
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| Format | Text, Technical Report |
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| Physical description | 1 PDF/A (2 MB), 17 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 | As the theoretical calculations indicated a possibility of the development of rudder flutter on CF-105, an experimental verification of the critical speed and frequency was required. A series of tests in the NAE 30 in. x 16 in. supersonic wind tunnel was performed on a fin model equipped with rudders of suitable density and hinge stiffness. |
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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. High Speed 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 | f5c30f68-d3ed-4f3e-9946-43306879ab74 |
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| Record created | 2021-06-03 |
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| Record modified | 2022-05-19 |
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