Record Details
| 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: |
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| 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)
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| 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 | ||||||