Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated ice
Author:
Affiliation:
1. Texas A&M University, College Station, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45096
Reference12 articles.
1. Helicopter rotor performance degradation in natural icing encounter
2. Performance degradation of propeller systems due to rime ice accretion
3. Experimental study of performance degradation of a model helicopter main rotor with simulated ice shapes
4. Performance degradation of a model helicopter main rotor in hover and forward flight with a generic ice shape
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2. Stall Mitigation and Lift Enhancement of NACA 0012 with Triangle-Shaped Surface Protrusion at a Reynolds Number of 105;SAE International Journal of Aerospace;2019-11-21
3. Numerical investigation of the unsteady aerodynamics of NACA 0012 with suction surface protrusion;Aircraft Engineering and Aerospace Technology;2019-11-21
4. Airfoil-Performance-Degradation Prediction Based on Nondimensional Icing Parameters;AIAA Journal;2013-11
5. Analytical and Experimental Determination of Airfoil Performance Degradation Due to Ice Accretion;4th AIAA Atmospheric and Space Environments Conference;2012-06-25
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