Penalization Method for Eulerian Droplet Impingement Simulations Toward Icing Applications-Reference-Cited by-同舟云学术

Penalization Method for Eulerian Droplet Impingement Simulations Toward Icing Applications

Published:2022-02 Issue:2 Volume:60 Page:641-653
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Lavoie Pierre¹^ORCID,Radenac Emmanuel²,Blanchard Ghislain²,Laurendeau Eric³,Villedieu Philippe²

Affiliation:

1. Polytechnique Montreal, Montreal, Quebec H3T 1J4, Canada

2. ONERA/DMPE, University of Toulouse, F-31055 Toulouse, France

3. Montreal Polytechnic, Montreal, Quebec H3T 1 J4, Canada

Funder

ONERA

The Canada Research Chair program

Natural Sciences and Engineering Research Council of Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060511

Reference32 articles.

1. WrightW. B.GentR. W.GuffondD. “DRA/NASA/ONERA Collaboration on Icing Research: Part II—Prediction of Airfoil Ice Accretion,” NASA CR–202349, 1997, https://ntrs.nasa.gov/citations/19970023937 [retrieved 11 Nov. 2021].

2. Aircraft icing

3. WrightW. B. “User’s Manual for LEWICE Version 3.2,” NASA CR 2008-214255, 2008, https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20080048307.pdf [retrieved 11 Nov. 2021].

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

5. An improved characteristic based volume penalization method for the Euler equations towards icing applications

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