| Auteur | Rechercher : Templin, R. J.1 |
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| Affiliation | - Conseil national de recherches Canada
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| Format | Texte, Mémorandum |
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| Description physique | 17 p. |
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| Sujet | Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; avion à réaction supersonique du Canada; intercepteur supersonique à ailes delta |
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| Résumé | 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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| Date de publication | 1955-03-24 |
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| Maison d’édition | National Research Council Canada. National Aeronautical Establishment. Aerodynamics |
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| Série | |
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| Est identique à | |
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| Langue | anglais |
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| Publications évaluées par des pairs | Non |
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| Exporter la notice | Exporter en format RIS |
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| Signaler une correction | Signaler une correction (s'ouvre dans un nouvel onglet) |
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| Identificateur de l’enregistrement | 5ccf94a8-daed-489c-8bb9-219bd28f9a52 |
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| Enregistrement créé | 2020-11-26 |
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| Enregistrement modifié | 2025-12-04 |
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