Anisogrid lattice structures – survey of development and application
Tóm tắt
Từ khóa
Tài liệu tham khảo
Poulsen CM. Geodetic construction. How the Vickers-Armstrong Wellington is built: solving novel and sometimes difficult production problems. Aircraft Production Part 1 1940:43–148; Part assembly of Wellington fuselages and wings: works layout and equipment. Aircraft Production 1940:180–88
Rutan, 1966, From concept chaos to clear concepts, SAMPE J., 32, 18
Mackay R. Wellington in action. Texas: Squadron/Signal Publication; 1986
Huybrechts SM, Hahn SE, Meink TE. Grid stiffened structures: survey of fabrication, analysis and design methods. In: Massard T, Vautrin A, editors. Proceedings of the 12th International Conference on Composite Materials (ICCM/12). Paris, France; July 1999 (Electronic version)
Duft BL. Method of making a filament wound sandwich core. US Patent No. 3, 300, 354 of January 24, 1967
Figger IE. Tetra-core. Shell Aviation News 1971; (391)
Renfield LW, Deo RB, Reniery GD. Continuous filament advanced composite isogrid: a promising design concept. In: Fibrous composites in structural design. New York: Plenum Press; 1980. p. 215–39
Kim TD, Koury JL, Telford KN, Tracy JJ, Harvey JA. Continuous fiber composite isogrid for launch vehicle applications. In: Miravete A, editor. Proceedings of the 9th International Conference on Composite Materials (ICCM/9). Madrid; July 1993; Vol.6, Composite properties and applications. University of Zaragoza; 1993, p. 101–7
Wang SS, Srinivasan S, Su KB, Dunham MG. A structural efficiency study of isogrid-stiffened fiber composite laminate shells: buckling and postbuckling analysis and experiments. In: Poursartip A, Street K, editors. Proceedings of the 10th International Conference on Composite Materials (ICCM/10). Canada; August 1995; Vol. 5, Structures. Woodhead Publishing Ltd.; 1995. p. 59–68
Slinchenko D, Verijenko VE, Lene F, Duvaut G. Optimum design of grid cylindrical structures using homogenised model. In: Massard T, Vautrin A, editors. Proceedings of the 12th International Conference on Composite Materials (ICCM/12). Paris, France; July 1999 (Electronic version)
Chen, 1996, Analysis and optimum design of composite grid structures, J. Compos. Mater., 30, 503, 10.1177/002199839603000405
Hou, 1998, Design, damage tolerance and filament wound attach fitting for launch vehicle, J. Adv. Mater., 30, 16
Hayashi, 1991, Buckling strength of cylindrical geodetic structures, Jpn–US Conf. Compos. Mater., Tokio, 428
Nosaki Y, Takamatsu H, Fukushima Y, Matsubara S. Development of CFRP spacecraft attach fitting. In: Proceedings of 13th International Symposium of Space Technology and Science. Tokyo; 1982. p. 373–78
Onoda, 1986, On optimal design of lattice cylinders, Trans. Jpn. Soc. Aeronaut. Space Sci., 29, 46
Vasiliev, 1993
Vasiliev VV, Pichkadze GP. Composite shells and plates with spatial reinforcement. In: Design, analysis, and testing of composite structures, vol. 9. Central Aerohydrodynamics Institute; 1982. p. 83–90 (in Russian)
Bunakov VA, Fedorov LV. Application of micropolar theory of elasticity to lattice structures. Mechanics of Solids (Proc. of Russian Academy of Sciences) 1994;(4):148–54 (in Russian)
Bunakov VA. Design of axially compressed composite cylindrical shells with lattice stiffeners. In: Vasiliev VV, Gurdal Z, editors. Optimal structural design. USA: Technomic Publishing Co.; 1999. p. 207–46
Vasiliev VV, Lopatin AV. Theory of lattice and stiffened composite shells. In: Nemirovskii YuV, editor. Mechanics of composite structures. Novosibirsk: Nauka; 1984. p. 31–6 (in Russian)
Zener, 1971
Bunakov VA, Protasov VD. Lattice composite structures. In: Mechanics and technical progress, Vol. 4: application of mechanics to technology. Moscow: Nauka; 1988. p. 273–86 (in Russian)