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Tests on a model of the working section of the proposed propulsion wind tunnel

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DOITrouver le DOI : https://doi.org/10.4224/40003959
AuteurRechercher : 1
Affiliation
  1. Conseil national de recherches Canada. Division de génie mécanique
FormatTexte, Mémorandum
Description physique12 p.
Résumé
In view of the unusual nature of the air flow to be expected in this tunnel, when wind and fan streams interact, it was thought desirable to test models of various types of working section. In order to obtain maximum speed from the available power, a 10' x 15’ working jet was assumed, with the wing spanning the 10’ dimension, leaving a 10’ span x 7 1/2’ high jet above it, and the same below it. A 9’ chord wing was assumed, with a 3’ dia. fan in it. The tests described covered various configurations of working section, divided into two main groups, namely, open-jet and closed-tunnel working sections.
Date de publication
Maison d’éditionNational Research Council Canada
Série
  • Laboratory Memorandum (National Research Council Canada. Division of Mechanical Engineering. Engine Laboratory), nº NRC-ENG-21 (25 mai 1960).
Langueanglais
Publications évaluées par des pairsNon
Exporter la noticeExporter en format RIS
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Identificateur de l’enregistrement99566bb2-2fc0-487f-8f5a-7eeab2959867
Enregistrement créé2026-02-13
Enregistrement modifié2026-02-13

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