Numerical Simulations for Ice Accretion on Rotors Using New Three-Dimensional Icing Model
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033986
Reference27 articles.
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4. MillerT. L.BondT. H. “Icing Research Tunnel Test of a Model Helicopter Rotor,” NASA TM-101978, 1989.
5. Experimental investigation of ice accretion on rotorcraft airfoils at high speeds
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