1、null nullcI|: 1006null2793( 2005) 03null0224null04 88c 9 ZE , A b(?,. 88c 9 m J. , 2005, 22(4).(编辑:薛永利)( 218:) ID 1 null LuchmannW A. Aerothermal ablative characterization of senulllected insulator candidatesR. AIAA 93null1857. 2 null Chow L. External insulation for tacticalmissile solid rocketmotor
2、 propulsion systems R. A IAA 89null2425. 3 null . - /p J.t , 1992, ( 3): 56. 4 null ) .p M .:, 1994. 5 null 2.+p M . Z: Z S/ ,1984. 6 null I. (/) M .:t, 1993. 7 null;.p p / M .:S,1994. 8 null . p J.t , 1996, ( 2):102null103.(编辑:刘红利)( 223:)dLq B/ S y wbBTBdL8q B/ y w#y wV8 Z$b ID 1 null Sm ith P J, W
3、 ilson R D. Damage tolerant composite w ingpanels for transport aircraft R. NASA Contractor Report,Boeing CommercialA irplane Company, 1985: 3951. 2 null Dow M B, Smith D L. Damage tolerant composite materialsproduced by stitching carbon fabrics C. Int. SAMPETechnullnicalCon.f, 1989, Series, 21: 595
4、null605. 3 null Cox B N. Delam ination and buckling in 3D composites J.J. CompositeM aterials, 1994, 28( 12): 1114null1126. 4 null Li Siping, Huang Yuying, Hu Yuanta,i ZhongW eifang. Anullnalysis on buckling and postnullbuckling of delam ination in 3Dcomposites J. Acta M echanica Solida Sinica., 199
5、7, 10( 3): 212null219. 5 null , ,Y. 3D B s J.%8 , 1997, 18( S): 94null99. 6 null , v, ._8q B Zs J. , 1998, 15( 4):145null150. 7 null , , v. 3D 8q B y wY J. , 1998, 15( 4):127null132. 8 null L iS, N ie J, Q ian J, Huang Y, Hu Y. Initial postnullbucklingand growth of a circular delam ination bridged by nonlinear finullbers J. ASM E J. App.l M ech., 2000, 67( 4): 777null784. 9 null , WyS, +M ,. y w J.%8p/ , 2000, 23( 1): 40null46.(编辑:吕耀辉)null227null2005 M9 ,: 88c 9 ZE3
