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Wind Tunnel Measured Effects on a Twin-Engine Short-Haul Transport Caused by Simulated Ice Accretions: Data ReportThe 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.
Document ID
19970023376
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Reehorst, Andrew (NASA Lewis Research Center Cleveland, OH United States)
Potapczuk, Mark (NASA Lewis Research Center Cleveland, OH United States)
Ratvasky, Thomas (NASA Lewis Research Center Cleveland, OH United States)
Laflin, Brenda Gile (NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1997
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.15:107419
E-10659
NASA-TM-107419
Accession Number
97N23718
Funding Number(s)
PROJECT: RTOP 548-20-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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