Decorative Laminates, Used Clothing, Rice, Sugar, Cement and Sand.
采購產品裝飾積層塑料板,二手的衣服, 大米, 糖, 水泥和沙子.
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Transverse cracking of matrix is a main damage type of cross - ply laminates.
基體橫向開裂是復合材料正交層板的主要損傷類型.
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Stress singularity and inhomogeneity in composite laminates . 6.
復合材料結構之應力奇異性相關問題.
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The three - dimensional exact solution methods for dynamic problems a finitely long piezoelectric composite laminates are studied.
有限長壓電層合板結構動態(tài)問題的三維精確解研究.
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The characteristics of interlayer metal have effect on the performance of whole laminates.
夾層金屬材料本身的性能對疊層材料整體的性能也有一定的影響.
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In composite laminates there are four basic failure modes: matrix cracking, delamination, fiber breakage and debonding.
復合材料層合板中存在四種基本的失效模式,即: 基體開裂 、 分層 、 纖維斷裂及脫粘.
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The behaviors and effective factors of laminates under flexural stress are analysed in this paper.
本文分析、討論了積層板材料,在彎曲應力下的各種性能及影響因素.
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The ideas and methods on the structure design of composite laminates are put forward.
從合層板的彎曲剛性出發(fā),提出了復合材料層合板的結構設計的思想和方法.
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These versatile laminates provide extremely high impact resistance and absorb total impact energy without spalling.
這些通用板材具有高抗沖擊性,能吸收所有沖擊能量而不碎裂.
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A comprehensively coupled thermo - piezoelectric - mechanical model of composite laminates with single surface bonded piezoelectricapplied loads, is developed.
本文針對一種單面粘貼壓電材料的復合材料層合板結構,建立了一種熱 - 機-電完全耦合模型.
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By means of velocity feedback control agolrithm the active vibration control of laminates is fulfilled.
并采用速度反饋控制實現了層合板的主動振動控制.
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The failure analysis methods for composite laminates have been also discussed in this paper.
本文還討論了復合材料中的失效分析方法.
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The direction stabilizer of aircraft can be improved by optimizing the composite laminates of vertical stabilizer.
通過優(yōu)化垂尾復合材料蒙皮鋪層體系,可以減少垂直尾翼的氣動變形,進而改善飛機的方向安定性.
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The rehabilitation of reinforced concrete structures with CFRP laminates is a new reinforcement technique.
碳纖維布加固混凝土結構是一種新型的結構加固方法.
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The given solution satisfies all fundamental equations of elasticity and continuity conditions between the laminates.
此解滿足層合板的基本方程和層間連續(xù)條件.
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