| Téléchargement | - Voir la version finale : The stability of fan-in-wing VTOL aircraft (from the power-plant aspect) (PDF, 2.4 Mio)
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| DOI | Trouver le DOI : https://doi.org/10.4224/40003793 |
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| Auteur | Rechercher : Fowler, H. S.1 |
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| Affiliation | - Conseil national de recherches Canada. Division de génie mécanique
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| Format | Texte, Mémorandum |
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| Description physique | 13 p. |
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| Résumé | The stability is considered during hovering flight of a 20,000 lbs. AUW aircraft as described by Galitzine with structure weights estimated on a basis described in a memo by Pocock. In the rolling stability case, a modified form of the aircraft with a high aspect ratio wing is compared with this low-aspect ratio design.
Fan control and response rates in hovering vertical stability ("heave") are discussed briefly, and the requirements in roll stabilization are examined, together with the merits of some possible control systems. |
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| Date de publication | 1961-12 |
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| Maison d’édition | National Research Council Canada |
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| Série | |
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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 | 121b4c83-24e7-4639-a09b-abfc733ba0aa |
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| Enregistrement créé | 2025-10-21 |
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| Enregistrement modifié | 2025-11-03 |
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