Citation: | Yan De, Yang Chao. Flight loads analysis of longitudinal maneuver using experimental aerodynamic forces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 253-256. (in Chinese) |
[1] 万志强,唐长红,邹丛青.柔性复合材料前掠翼飞机静气动弹性分析[J].复合材料学报,2002,19(5):118-124 Wan Zhiqiang,Tang Changhong,Zou Congqing.Static aeroelastic characteristics analysis of a flexible forward-swept composite aircraft[J].Acta Materiae Compositae Sinica,2002,19(5):118-124(in Chinese) [2] MSC.Nastran version 2001 release guide[M]. Los Angeles:MSC Software Corporation,2001:127-165 [3] 邓立冬,李天.柔性飞机的非线性飞行载荷计算研究[J].飞行力学, 2004,22(4):85-88 Deng Lidong,Li Tian.Research of nonlinear flight loads calculation on a flexible aircraft[J].Flight Dynamics,2004,22(4):85-88(in Chinese) [4] 万志强,邓立东,杨超,等.基于非线性试验气动力的飞机静气动弹性响应分析[J].航空学报,2005,26(4):439-445 Wan Zhiqiang,Deng Lidong,Yang Chao,et al.Aircraft static aeroelastic response analysis based on nonlinear experimental aerodynamic data[J].ACTA Aeronautica et Astronautica Sinica,2005,26(4):439-445(in Chinese) [5] Rodden W P,Johnson E H.MSC/Nastran aeroelastic analysis user-s guide V68[M].Los Angeles:MSC Software Corporation,1994:44-65 [6] Harder R L,Desmarais R N.Interpolation using surface spline[J]. Journal of Aircraft, 1972,9(2):189-191 [7] 林成森.数值计算方法(下册) [M].北京:科学出版社,2000:160-166 Lin Chengsen.Numerical computation method[M].Beijing:Science Press,2000:160-166(in Chinese)
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