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OverviewThe purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tunnel test that examined icing effects on a 1/8 scale twin-engine short-haul jet transport model. Presented in this document are summary data from the major configurations tested. The entire test database in addition to ice shape and model measurements is available as a data supplement in CD-ROM form. Data measured and presented are: wing pressure distributions, model force and moment, and wing surface flow visualization. Reehorst, Andrew and Potapczuk, Mark and Ratvasky, Thomas and Laflin, Brenda Gile Glenn Research Center; Langley Research Center FLOW VISUALIZATION; JET AIRCRAFT; PRESSURE DISTRIBUTION; ICE FORMATION; ICE; TRANSPORT AIRCRAFT; CD-ROM; WINGS... Full Product DetailsAuthor: National Aeronaut Administration (Nasa)Publisher: Createspace Independent Publishing Platform Imprint: Createspace Independent Publishing Platform Dimensions: Width: 21.60cm , Height: 0.60cm , Length: 27.90cm Weight: 0.263kg ISBN: 9781723488405ISBN 10: 1723488402 Pages: 104 Publication Date: 23 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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