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Record Details

Record 5 of 10613
Wind Tunnel Measured Effects on a Twin-Engine Short-Haul Transport Caused by Simulated Ice Accretions: Data Report
Offline Availability: Go to Request Form
Author and Affiliation:
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)
Abstract: The 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.
Publication Date: May 01, 1997
Document ID:
20140000920
(Acquired Feb 27, 2014)
Subject Category: AIR TRANSPORTATION AND SAFETY
Report/Patent Number: NASA-TM-107419, E-10659
Document Type: Data Set
Publication Information: (SEE 1997034739)
Contract/Grant/Task Num: RTOP 548-20-23
Financial Sponsor: NASA Lewis Research Center; Cleveland, OH, United States
Description: In English; CD-ROM contains data files
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: FLOW VISUALIZATION; JET AIRCRAFT; PRESSURE DISTRIBUTION; ICE FORMATION; ICE; TRANSPORT AIRCRAFT; WINGS; DATA BASES
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