New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils-Reference-Cited by-同舟云学术

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New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils

Published:2021-01 Issue:1 Volume:59 Page:250-262
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Min Seungin¹,Yee Kwanjung¹

Affiliation:

1. Seoul National University, Seoul 08826, Republic of Korea

Funder

Korea Agency for Infrastructure Technology Advancement (KAIA), funded by the Ministry of Land, Infrastructure, and Transport

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference29 articles.

1. RuffG. A.BerkowitzB. M. “User’s Manual for the NASA Lewis Ice Accretion Prediction Code (LEWICE),” NASA CR-185129, 1990.

2. CebeciT.BradshawP., Physical and Computational Aspects of Convective Heat Transfer, Springer-Verlag, New York, 1984, pp. 58–61.

3. WrightW. “Advancements in the LEWICE Ice Accretion Model,” NASA CR-191019, 1993.

4. Quasi-Steady Convergence of Multistep Navier–Stokes Icing Simulations

5. Development of a Second Generation In-Flight Icing Simulation Code

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