FENSAP-ICE: Eulerian Modeling of Droplet Impingement in the SLD Regime of Aircraft Icing-Reference-Cited by-同舟云学术

FENSAP-ICE: Eulerian Modeling of Droplet Impingement in the SLD Regime of Aircraft Icing

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Honsek Raimund¹,Habashi Wagdi G.¹

Affiliation:

1. McGill University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-465

Reference25 articles.

1. Bragg, M.B. "Aircraft AerodynamicEffects duetoLargeDroplet IceAccretions", AIAA-96-0932

2. Brahimi, M.T., Tran, P., Tezok, F.,Paraschivoiu, I."Aircraft Icing dueto Supercooled LargeDroplets", pp.533-544

3. Brahimi, M.T., Tran, P., Chocron, D., Tezok, F., Paraschivoiu, I. "Effect of Supercooled Large Droplets on Ice Accretion Characteristics", AIAA-97-0306

4. Tan, S.C.,Papadakis, M."General Effects of LargeDroplet Dynamics on IceAccretion Modeling", AIAA-2003-0392

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