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�������պ����ѧѧ�� 2006, Vol. 32 Issue (06) :671-674    DOI:
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��Խ, ����, ���人*
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Transient analytical method of vane forcing response under stator-rotor wake influence
Meng Yue, Li Lin, Li Qihan*
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� Rotor blade forcing response problems due to the wake of front vane row was analyzed. A transient analytical method was presented for blade forcing response. Then displacement and stress could be predicted. The analysis of three-dimension unsteady flow field was performed with NUMECA to provide the wake influence force and the pressure was introduced into calculating structure dynamics(CSD). Structure analysis was performed by finite element package ANSYS using transient analysis type. Force boundary condition was written with ANSYS parametric design language(APDL), a scripting language for ANSYS. The displacement and stress under different rotate speed were calculated. Then compared them with Compbell method. For transient analytical method, whether flow field or structure analysis were both presented with well-rounded software, so it’s easy for using in engineering field.
Keywords�� wake influence   forcing response   transient analytical method     
Received 2005-07-01;
About author: �� Խ(1978-),Ů,����������,��ʿ��, mengyue@sjp.buaa.edu.cn.
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��Խ, ����, ���人.β�����������ҶƬǿ����Ӧ˲̬��������[J]  �������պ����ѧѧ��, 2006,V32(06): 671-674
Meng Yue, Li Lin, Li Qihan.Transient analytical method of vane forcing response under stator-rotor wake influence[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(06): 671-674
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2006/V32/I06/671
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