| Téléchargement | - Voir la version finale : Effects of compressibility in wing-immersed pans for lifting VTOL aircraft (PDF, 3.5 Mio)
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| DOI | Trouver le DOI : https://doi.org/10.4224/40003983 |
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| Auteur | Rechercher : Galitzine, N.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 | 18 p. |
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| Résumé | In reference 1 a rather simplified theory of axial-flow wing-immersed lifting fans for VTOL aircraft was presented for the purpose of preliminary design and size and weight estimation.
At the time of writing disc loadings of about 200-400 lb/ ft²were considered, and it was felt that the effects of compressibility on the design of the fans could be neglected.
Reference 2 investigated the effects of fan disc loading on the weight and cost of VTOL powerplants with gross disc loading varying from 200 to 1000 lb/ ft². The resulting curves of weight and cost were lowest but rather flat in the 500-1000 lb/ ft² region, showing optima lying between 500 and 750 lb/ ft² depending upon the criteria of either weight or cost. |
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| Date de publication | 1960-06-23 |
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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 | c638aa70-b0eb-4656-aa2b-0ca71b31a8f7 |
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| Enregistrement créé | 2026-02-20 |
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| Enregistrement modifié | 2026-02-20 |
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