Aerodynamic Simulation of Runback Ice Accretion

Author:

Broeren Andy1,Whalen Edward2,Busch Greg3,Bragg Michael3

Affiliation:

1. NASA Glenn Research Center

2. The Boeing Company

3. University of Illinois at Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Reference62 articles.

1. α 4.13deg.0.02deg.0.48% ClBalance 0.556 -0.00086 -0.16% CmBalance -0.0015 -0.00027 -17.4%

2. Cp -0.962 -0.0045 -0.47% CdWake 0.0071 -0.00014 -1.9% Table2 Estimated Experimental Uncertaintiesfor Measurements inthe ONERAF1WindTunnel.

3. Fig.3 Photograph ofNG0671 runback ice accretion casting, top-upper-surfaceridge, bottom-lowersurface ridge. Fig.4 Completed installationofrunbackridge simulationNG0671ontheleading edgeof thefullscaleNACA23012 model. x/c 0.00 0.05 0.10 0.15 0.20 -0.05 D. SubscaleModel Ice-ShapeSimulation Methods

4. α(deg) -8 -6 -4 -2 0 2 4 6 8 10 12 14 16 18 20 -0.8 -0.6 -0.4 -0.2 0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0

5. α(deg) -8 -6 -4 -2 0 2 4 6 8 10 12 14 16 18 20 -0.8 -0.6 -0.4 -0.2 0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0

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1. Ice Shape Classification for Swept Wings;AIAA AVIATION 2020 FORUM;2020-06-08

2. Validation of 3-D Ice Accretion Measurement Methodology for Experimental Aerodynamic Simulation;6th AIAA Atmospheric and Space Environments Conference;2014-06-13

3. Aerodynamic Classification of Swept-Wing Ice Accretion;5th AIAA Atmospheric and Space Environments Conference;2013-06-22

4. Aerodynamics of a Swept Wing with Ice Accretion at Low Reynolds Number;30th AIAA Applied Aerodynamics Conference;2012-06-25

5. Ice Shape Characterization to Aid in Replicating Ice Shapes for Subsequent Analysis;AIAA Atmospheric and Space Environments Conference;2010-06-14

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