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Wind tunnel measured effects on a twin-engine short-haul transport caused by simulated ice accretions
Author(s) -
Andrew Reehorst,
Mark Potapczuk,
Thomas Ratvasky,
Brenda Gile Laflin
Publication year - 1996
Publication title -
38th aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1996-871
Subject(s) - wind tunnel , environmental science , meteorology , geology , aerospace engineering , atmospheric sciences , engineering , physics
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.

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