| Author | Search for: Templin, R. J.1 |
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| Affiliation | - National Research Council of Canada
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| Format | Text, Memorandum |
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| Physical description | 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 | This memorandum attempts to deduce the effects of adding arbitrary camber and twist to a wing of given plan form, at least as far as these effects can be determined without involving complex assumptions and lifting surface calculations. The analysis is too simple to provide a method of design of cambered wings, but it does explain qualitatively their behaviour. It also suggests methods of assessing test results, and of comparing the results of cambered wings designed for different flight conditions. |
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| Publication date | 1955-03-24 |
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| Publisher | National Research Council of Canada. National Aeronautical Establishment. Aerodynamics |
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| Series | |
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| Is identical to | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 5ccf94a8-daed-489c-8bb9-219bd28f9a52 |
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| Record created | 2020-11-26 |
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| Record modified | 2025-03-11 |
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