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�������պ����ѧѧ�� 2011, Vol. 37 Issue (1) :49-53    DOI:
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Convective heat transfer analysis of anti-icing surface
Song Xin, Lin Guiping, Bu Xueqin*
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

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Abstract�� An integral analysis of momentum and thermal boundary-layers was used to determine the convective heat transfer coefficient on two-dimensional airfoils with thermal anti-ice system. The objective are to implement two different boundary-layer models: one assumed isothermal surface with prensence of a abrupt laminar-turbulent transition, while the other considered the boundary-layers over a non-isothermal surface with a smooth laminar-turbulent transition region. The onset and length of laminar-turbulent transition was estimated by classic empirical correlations. The surface equilibrium temperature distribution was predicted by an integrated airoil leading-edge interior-exterior thermodynamic analysis, compared to the literature and experimental data. The results indicate a validity of using boundary-layer anaylysis with smooth laminar-turbulent transition in predicting anti-icing convective heat transfer and surface temperature, but the simulation shows that surrounding static pressure has a large effect on the results accuracy.
Keywords�� boundary-layer integral analysis   convective heat transfer coefficient   surface temperature     
Received 2009-11-23;
About author: �� ܰ(1986-),Ů,����������,˶ʿ��,songxin0110@163.com.
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��ܰ, �ֹ�ƽ, ��ѩ��.��������Ķ������ȼ������[J]  �������պ����ѧѧ��, 2011,V37(1): 49-53
Song Xin, Lin Guiping, Bu Xueqin.Convective heat transfer analysis of anti-icing surface[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2011,V37(1): 49-53
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