Ice Accretion on Helicopter Fuselage Considering Rotor-Wake Effects
Author:
Affiliation:
1. Seoul National University, Seoul 151-742, Republic of Korea
2. Pusan National University, Busan 609-735, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033830
Reference26 articles.
1. Helicopter icing
2. BaileyN., Helicopter Pilot’s Manual: Principles of Flight and Helicopter Handling, The Crowood Press, Ramsbury, England, U.K., 2014, pp. 99–101.
3. SzilderK. “Numerical Simulation of Ice Formation on a Helicopter Fuselage,” Soc. of Automotive Engineers TP-2007-01-3308, 2007. doi:10.4271/2007-01-3308
4. FENSAP-ICE-Unsteady: Unified In-Flight Icing Simulation Methodology for Aircraft, Rotorcraft, and Jet Engines
5. Numerical and Experimental Investigation of Ice Accretion on Rotorcraft Engine Air Intake
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