| Auteur | Rechercher : Pocock, P. J.1; Rechercher : Westell, J. R.1 |
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| Affiliation | - Conseil national de recherches Canada
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| Format | Texte, Rapport technique |
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| Description physique | 22 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 | The induced drag factor for delta wings with approximately 60 degrees of leading edge sweepback is found to be affected greatly by the aerofoil section shape. For thin sections (e.g. 5 percent) or thick sections with sharp noses the induced drag factor varies between 0.40 and 0.50. For thick sections (e.g. 10 percent) values of 0.8 and 0.9 can be obtained. The above results apply for Reynolds' Numbers of 4 million or greater. On the basis of limited data it appears that the induced drag factor for thin sectioned wings does not change over the subsonic Mach Number range. |
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| Date de publication | 1954-07-28 |
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| Maison d’édition | National Research Council Canada. National Aeronautical Establishment. Aerodynamics Laboratory |
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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 | 15207125-32b1-4214-a2aa-f6d9d6361808 |
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| Enregistrement créé | 2020-11-26 |
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| Enregistrement modifié | 2025-12-05 |
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