Quasi-Steady Convergence of Multistep Navier–Stokes Icing Simulations-Reference-Cited by-同舟云学术

Quasi-Steady Convergence of Multistep Navier–Stokes Icing Simulations

Published:2013-07 Issue:4 Volume:50 Page:1261-1274
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hasanzadeh K.¹,Laurendeau E.¹,Paraschivoiu I.¹

Affiliation:

1. Département de Génie Mécanique, École Polytechnique, Centre-Ville, Montréal H3C 3A7, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032197

Reference26 articles.

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2. WrightW. B. “Users Manual for the NASA Glenn Ice Accretion Code LEWICE Version 2.0,” NASA CR-209409, Sept. 1999.

3. WrightW.GentR. W.GuffondD. “DRA/NASA/ONERA Collaboration on Icing Research, Part II-Prediction of Airfoil Ice Accretion,” NASA CR-202349, May 1997.

4. Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed

5. KreegerR. E.WrightW. B. “The Influence of Viscous Effects on Ice Accretion Prediction and Airfoil Performance Predictions,” NACA TM-2005-213593, March 2005.

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