The Embraer-170 and -190 Natural Icing Flight Campaigns: Keys to Success
Author:
Affiliation:
1. Leading Edge Atmospherics, LLC
2. EMBRAER
3. Science Engineering Associates, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-264
Reference4 articles.
1. 1Wright,W.,2005.ValidationResultsforLEWICE3.0.AIAA-2005-1243
2. Wind Tunnel Measurements of the Response of Hot-Wire Liquid Water Content Instruments to Large Droplets
3. 4Bernstein, B.C., 2005: An inferred European climatology of icing conditions, including supercooled large droplets. FAA/DOT AR-05/24. Federal Aviation Administration Technical Report. Available from the National Technical Information Service(NTIS),Springfield,Virginia.
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1. Design and Research on the Refit Scheme for Natural Icing Flight Test of Large Civil Aircraft;Journal of Physics: Conference Series;2024-06-01
2. Icing on Full-Scale Swept Wings in Flight and Icing Wind Tunnel;Journal of Aircraft;2022-11
3. Real-Time Regional Jet Comprehensive Aeroicing Analysis via Reduced-Order Modeling;AIAA Journal;2016-12
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