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OverviewInducer and impellar base geometries were defined for a fuel pump for a generic generator cycle. Blade surface data and inlet flowfield definition are available in sufficient detail to allow computational fluid dynamic analysis of the two components. Eastland, A. H. J. and Dodson, H. C. Unspecified Center NASA-CR-184252, NAS 1.26:184252, RI-RD-91-193, REPT-91RC11706 NAS8-38863... Full Product DetailsAuthor: National Aeronaut Administration (Nasa)Publisher: Createspace Independent Publishing Platform Imprint: Createspace Independent Publishing Platform Dimensions: Width: 21.60cm , Height: 1.20cm , Length: 27.90cm Weight: 0.549kg ISBN: 9781724242259ISBN 10: 1724242253 Pages: 232 Publication Date: 25 July 2018 Audience: General/trade , General Format: Paperback Publisher's Status: Active Availability: Available To Order We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately. Table of ContentsReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |
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