Numerical Simulation of In-Flight Icing of Rotorcraft
Author:
Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-64725-4_10-1
Reference76 articles.
1. Açıkgöz MB, Aslan AR (2016) Dynamic mesh analyses of helicopter rotor–fuselage flow interaction in forward flight. J Aerosp Eng 29(6)
2. Ahn GB, Jung KY, Myong RS, Shin HB, Habashi WG (2015) Numerical and experimental investigation of ice accretion on rotorcraft engine air intake. AIAA J Aircraft 52(3):903–909
3. Aliaga CN, Aubé MS, Baruzzi GS, Habashi WG (2011a) FENSAP-ICE-unsteady: unified in-flight icing simulation methodology for aircraft, rotorcraft, and jet engines. AIAA J Aircraft 48(1):119–126
4. Aliaga CN, Aubé MS, Baruzzi GS, Habashi WG (2011b) FENSAP-ICE-Unsteady: unified in-flight icing simulation methodology for aircraft, rotorcraft, and jet engines. AIAA J Aircraft 48(1):119–126
5. Bain J, Cajigas J, Sankar L, Flemming RJ, Aubert R (2010) Prediction of rotor blade ice shedding using empirical methods, AIAA Paper 2010–7985
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