Scallop ice shape characteristics of swept wing based on large-scale icing wind tunnel experiment
Author:
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference45 articles.
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4. Von Glahn UH, Gray VH. Effect of ice formations on section drag of swept NACA 63A-009 airfoil with partial-span leading–edge slat for various modes of thermal ice protection. Washington D.C.: NACA; 1954. Report No.: NACA RM E53J30.
5. Vargas M, Tsao JC. Time-sequence observations of the formation of ice accretions on swept wings. Proceedings of the 46th AIAA aerospace sciences meeting and exhibit. Reston: AIAA; 2008.
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