| Autre titre | Supersonic wind tunnel tests on the effects of engine-off operation on lateral characteristics of the C-105 aircraft |
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| Auteur | Rechercher : LaBerge, J. G.1; Rechercher : Boyer, D. W.1 |
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| Affiliation | - Conseil national de recherches Canada
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| Format | Texte, Mémorandum |
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| Description physique | 38 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 effect of blocking completely or partially one engine intake on the side force and yawing moment of the C-105 aircraft was investigated at supersonic speeds. A 1/80 scale model was tested in the 10 inch tunnel, the force and moment measurements being taken at a Mach number of 2.04. Schlieren photographs are presented for Mach numbers of 1.64 and 2.04.
Over the whole range of yaw angles explored complete blockage of one intake resulted in a yawing moment (ΔCₙ =0.001) tending to put the blocked intake on the windward side of the fuselage. |
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| Date de publication | 1955-10-24 |
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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 | 8298cd76-0f77-40ac-998f-e39b74eabe7c |
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| Enregistrement créé | 2020-11-26 |
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| Enregistrement modifié | 2025-12-04 |
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