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An Experimental Study of Stresses at the Interface of Propellant Grains and Motor Cases Due to Thermal Loading of the Shrinkage Type

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Tests are reported which show that, using the bonding knife-edged technique, the same distributions of stresses can be obtained in a rectangular two-dimensional rubber plate bonded to a metal strip, as in the central plane of a square slab with the same ratio of height to length as the rubber specimen. (Author)

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作者
Durelli, A. J.; Parks, V. J.;
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年度 1965
页码 p.1-2
总页数 2
原文格式 PDF
正文语种 eng
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关键词
Rocket propellant grains ; Rocket cases ; Solid rocket propellants ; Surface properties ; Stresses ; Bonding ; Rubber ; Models(Simulations) ; Photoelasticity ; Photographic analysis ; Deformation ; Simulation ; Epoxy plastics ; Model tests;

机译：火箭推进剂颗粒;火箭弹;固体火箭推进剂;表面特性;应力;粘结;橡胶;模型（模拟）;光弹性;摄影分析;变形;模拟;环氧塑料;模型试验;

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1. Experimental studies of the plasma-propellant interface for electrothermal-chemical launchers [J] . Edwards C.M., Bourham M.A. IEEE Transactions on Magnetics . 1995,第1期

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3. A multilayered thick cylindrical shell under internal pressure and thermal loads applicable to solid propellant rocket motors [J] . K.Renganathan, B.Nageswara Rao, M.K.Jana Forschung im Ingenieurwesen . 2000,第2期

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5. Experimental study of mixing and combustion processes in a solid propellant ducted rocket motor. [D] . Chuang, Chin-Lung. 1989

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8. An Experimental Study of Stresses at the Interface of Propellant Grains and Motor Cases Due to Thermal Loading of the Shrinkage Type [R] . Durelli, A. J., Parks, V. J. 1965

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An Experimental Study of Stresses at the Interface of Propellant Grains and Motor Cases Due to Thermal Loading of the Shrinkage Type

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