Surface Roughness and Heat Transfer Improved Predictions for Aircraft Ice-Accretion Modeling-Reference-Cited by-同舟云学术

Surface Roughness and Heat Transfer Improved Predictions for Aircraft Ice-Accretion Modeling

Published:2017-04 Issue:4 Volume:55 Page:1318-1331
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Han Yiqiang¹,Palacios Jose²

Affiliation:

1. Clemson University, Clemson, South Carolina 29634

2. Pennsylvania State University, University Park, Pennsylvania 16802

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055217

Reference34 articles.

1. RuffG.BerkowitzB. “Users Manual for the NASA Lewis Ice Accretion Prediction Code (LEWICE), ” NASA CR-185129, 1990.

2. WrightW. “Advancements in the LEWICE Ice Accretion Model,” NASA CR-191019, 1993.

3. NeelC.BergrunN.JukoofD.SchlaffB. “The Calculation of the Heat Required for Wing Thermal Ice Prevention in Specified Icing Conditions,” NACA TN-1472, 1947.

4. GelderT.LewisJ. “Comparison of Heat Transfer from Airfoil in Natural and Simulated Icing Conditions,” NACA TN-2480, 1951.

5. NewtonJ.Van FossenG.PoinsatteP.DeWittK. “Measurement of Local Convective Heat Transfer Coefficients from a Smooth and Roughened NACA-0012 Airfoil: Flight Test Data,” NASA TM-100284, 1988.

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