Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing-Reference-Cited by-同舟云学术

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Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing

Published:2020-03 Issue: Volume:98 Page:105659
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Prince Raj L.,Yee K.,Myong R.S.

Funder

National Research Foundation of Korea

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference61 articles.

1. Safety Advisor: Aircraft Icing;Landsberg,2008

2. Subsonic aircraft safety icing study;Jones,2008

3. Ice accretion and performance degradation calculations with LEWICE/NS;Potapczuk,1993

4. Validation Results for LEWICE 3.0;Wright,2005

5. Toward real-time aero-icing simulation of complete aircraft via FENSAP-ICE;Nakakita;J. Aircr.,2010

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1. A numerical simulation of the distribution and the variation law of the liquid water content in icing wind tunnel;Applied Thermal Engineering;2024-01

2. Ice sensitivity analysis of different airfoils;Journal of Physics: Conference Series;2024-01-01

3. Numerical Investigation on Intermittent Maximum Ice Accretion and Aerodynamic Performances of RG-15 Aerofoil at Low Reynolds Number;Aerospace;2023-12-21

4. Numerical Simulation and Meta Model of Rotorcraft Electrothermal Ice Protection Systems;Handbook of Numerical Simulation of In-Flight Icing;2023-12-12

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