An Experimental Investigation on the Unsteady Heat Transfer Process Over an Ice Accreting NACA 0012 Airfoil
Author:
Affiliation:
1. Iowa State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0035
Reference21 articles.
1. Measurements of local convective heat transfer coefficients on ice accretion shapes
2. The effect of initial ice roughness on airfoil aerodynamics
3. Heat and mass transfer during ice accretion on aircraft wings with an improved roughness model
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1. Utilization of Thermal Effect Induced by Plasma Generation for Aircraft Icing Mitigation;AIAA Journal;2018-03
2. Effect of square dimples on the temperature distribution and heat transfer coefficient of an NACA0012 airfoil;International Journal of Ambient Energy;2018-01-25
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