Evaluation of a Subgrid-Scale Computational Fluid Dynamics Model for Ice Roughness-Reference-Cited by-同舟云学术

Evaluation of a Subgrid-Scale Computational Fluid Dynamics Model for Ice Roughness

Published:2019-03 Issue:2 Volume:56 Page:787-799
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hanson David R.¹,Kinzel Michael P.¹

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16801

Funder

US Government

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035060

Reference42 articles.

1. Effects of leading-edge ice accretion geometry on airfoil performance

2. WrightW. “User’s Manual for LEWICE Version 3.2,” NASA CR-2008-214255, 2008, https://ntrs.nasa.gov/search.jsp?R=20080048307 [retrieved 2018].

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

4. The Influence of Viscous Effects on Ice Accretion Prediction and Airfoil Performance Predictions

5. WrightW. B.RutkowskiA. “Validation Results for LEWICE 2.0,” NASA CR-1999-208690, Cleveland, OH, Jan. 1999, https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990021235.pdf [retrieved 2018].

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