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�������պ����ѧѧ�� 2002, Vol. 28 Issue (5) :570-573    DOI:
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����1, ����1, ����2*
1. �������պ����ѧ �����������Ӧ����ѧϵ;
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Loading Spectra Development for Special Structural Members of Fighter
LIU Xiao-dong1, LIU Wen-ting1, WANG Zheng2*
1. Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics;
2. Chengdu Aircraft Design and Research Institute

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Abstract�� The approach and specialties of loading spectra development using maneuvers simulation technique for new-design aircraft were introduced in brief. Onthe above basis, the approach and key-points of developing stress/pressure spectrum for integral tank, gusts and sideslip spectrum for vertical tail were presented in detail. One key step of developing stress/pressure spectrum for integral tank is to calculate the pressure of the tank in all loading cases, and the G-A-G cycle should be taken into account for the analysis spectrum of the tank. The loading spectrum of the vertical tail is obtained by not only the simulation of maneuvers but also some statistical measurements.
Keywords�� fighter aircraft   loading spectrum   flight simulation   special component spectrum     
Received 2001-02-26;
About author: ��С��(1965-),��,������,��ʿ��,100083,����.
��С��, ����, ����.�߻������ⲿ������غ��ױ��Ƽ���[J]  �������պ����ѧѧ��, 2002,V28(5): 570-573
LIU Xiao-dong, LIU Wen-ting, WANG Zheng.Loading Spectra Development for Special Structural Members of Fighter[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2002,V28(5): 570-573
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2002/V28/I5/570
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