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�������պ����ѧѧ�� 2009, Vol. 35 Issue (6) :692-696    DOI:
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���ģ����AEDC������Ч�Ե���֤
��ʿ�1, �麣��2, ������2*
1. �������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100191;
2. �������պ����ѧ �ѧԺ, ���� 100191
Icing simulation and evaluation of AEDC method
Chang Shinan1, Hong Haihua2, Zhang Yuzhu2*
1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
2. School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

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Abstract�� The arnold engineering development center (AEDC) icing scaling method was introduced and validated through numerical simulation. By icing modeling software, icing numerical simulations were performed for NACA0012 airfoil and its 1/2 and 1/3 scale models, cylinder and its 1/2 scale model. Flow field, droplets impingement and ice accretion computations were all included in the simulations. Scaling icing conditions were chosen according to AEDC method. The results show that the reference and scaling icing process have a wonderful similarity. It can be concluded that the AEDC method is effective and icing numerical simulation can be used in icing similarity research.
Keywords�� icing scaling   theory of similarity   numerical simulation     
Received 2008-05-05;
About author: ��ʿ�(1968-),Ů,ɽ���ܴ���,������,snchang99@sina.com.
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��ʿ�, �麣��, ������.���ģ����AEDC������Ч�Ե���֤[J]  �������պ����ѧѧ��, 2009,V35(6): 692-696
Chang Shinan, Hong Haihua, Zhang Yuzhu.Icing simulation and evaluation of AEDC method[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2009,V35(6): 692-696
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2009/V35/I6/692
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