Penalization Method for Eulerian Droplet Impingement Simulations Toward Icing Applications

Author:

Lavoie Pierre1ORCID,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

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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