標(biāo)題: Titlebook: Buckling and Postbuckling of Composite Plates; G. J. Turvey,I. H. Marshall Book 1995 Chapman & Hall 1995 buckling.deformation.finite eleme [打印本頁(yè)] 作者: 不足木 時(shí)間: 2025-3-21 17:43
書(shū)目名稱Buckling and Postbuckling of Composite Plates影響因子(影響力)
書(shū)目名稱Buckling and Postbuckling of Composite Plates影響因子(影響力)學(xué)科排名
書(shū)目名稱Buckling and Postbuckling of Composite Plates網(wǎng)絡(luò)公開(kāi)度
書(shū)目名稱Buckling and Postbuckling of Composite Plates網(wǎng)絡(luò)公開(kāi)度學(xué)科排名
書(shū)目名稱Buckling and Postbuckling of Composite Plates被引頻次
書(shū)目名稱Buckling and Postbuckling of Composite Plates被引頻次學(xué)科排名
書(shū)目名稱Buckling and Postbuckling of Composite Plates年度引用
書(shū)目名稱Buckling and Postbuckling of Composite Plates年度引用學(xué)科排名
書(shū)目名稱Buckling and Postbuckling of Composite Plates讀者反饋
書(shū)目名稱Buckling and Postbuckling of Composite Plates讀者反饋學(xué)科排名
作者: 強(qiáng)制令 時(shí)間: 2025-3-21 21:41 作者: 積習(xí)已深 時(shí)間: 2025-3-22 01:33 作者: Acquired 時(shí)間: 2025-3-22 06:33 作者: 持久 時(shí)間: 2025-3-22 09:37 作者: 食料 時(shí)間: 2025-3-22 14:26
Landschaften der Bundesrepublikintense efforts because of the extended use of fibrous composites in aerospace, automotive, shipbuilding and other industries, and the need to establish the practical limits of the load-carrying capability of structures made from these materials. The approximate analytical techniques which have been作者: 使殘廢 時(shí)間: 2025-3-22 18:56 作者: HIKE 時(shí)間: 2025-3-23 01:03 作者: 低三下四之人 時(shí)間: 2025-3-23 02:41 作者: Cytology 時(shí)間: 2025-3-23 07:42 作者: 哀求 時(shí)間: 2025-3-23 10:55 作者: NEEDY 時(shí)間: 2025-3-23 15:40
https://doi.org/10.1007/978-1-349-86035-7. Design parameters such as layer thicknesses and ply angles can be employed to great effect to achieve an optimized structure with improved weight and stiffness characteristics. This chapter deals with the lay-up optimization of laminated plates subject to buckling loads. A survey of the subject is作者: 皺痕 時(shí)間: 2025-3-23 20:37
Understanding the good and the bad,This chapter is a review of the AFIT work and will discuss both its experimental and analytical features. Other organizations have pursued similar research [., .] and the AFIT work has cited their findings. AFIT is the only organization that has continued to explore many of the intricacies of this i作者: Jejune 時(shí)間: 2025-3-23 23:54 作者: 獨(dú)白 時(shí)間: 2025-3-24 05:46 作者: 持續(xù) 時(shí)間: 2025-3-24 09:16 作者: 流浪 時(shí)間: 2025-3-24 10:48
Shear deformation and sandwich configurationClassical plate theory (CPT) is generally credited to Kirchhoff over 125 years ago.作者: Tracheotomy 時(shí)間: 2025-3-24 16:03 作者: TAG 時(shí)間: 2025-3-24 19:26
William Buchanan BSc, CEng, Phdimportance. For example, composite plate-like subcomponents with cut-outs are being considered for use in many types of aerospace structures owing to their high stiffness-to-weight and strength-to-weight properties. These properties could ultimately yield substantial weight savings for aircraft structures.作者: Endemic 時(shí)間: 2025-3-25 03:03
http://image.papertrans.cn/b/image/191492.jpg作者: humectant 時(shí)間: 2025-3-25 07:16 作者: 坦白 時(shí)間: 2025-3-25 10:24
Series and Ritz-type buckling analysessis of buckling analysis of plate elements. The series solution gives us useful physical insights into the problems and accurate numerical results for the buckling loads of plates. The results obtained from the series-type solution, therefore, provide good data to compare with those obtained by nume作者: cruise 時(shí)間: 2025-3-25 14:36
Finite element buckling and postbuckling analysesintense efforts because of the extended use of fibrous composites in aerospace, automotive, shipbuilding and other industries, and the need to establish the practical limits of the load-carrying capability of structures made from these materials. The approximate analytical techniques which have been作者: choroid 時(shí)間: 2025-3-25 18:24 作者: deadlock 時(shí)間: 2025-3-25 20:07 作者: PTCA635 時(shí)間: 2025-3-26 03:23 作者: Gleason-score 時(shí)間: 2025-3-26 05:25 作者: 古老 時(shí)間: 2025-3-26 10:54
Delamination buckling of flat laminatesthe same time, this demand has forced upon him very sophisticated methods of testing, analysis and design, as well as of fabrication and manufacturing. The recent explosive progress in the production and use of composite materials has pointed toward the clear possibility of man creating specific mat作者: 外星人 時(shí)間: 2025-3-26 13:23
Lay-up optimization of laminated plates under buckling loads. Design parameters such as layer thicknesses and ply angles can be employed to great effect to achieve an optimized structure with improved weight and stiffness characteristics. This chapter deals with the lay-up optimization of laminated plates subject to buckling loads. A survey of the subject is作者: 季雨 時(shí)間: 2025-3-26 20:07 作者: overrule 時(shí)間: 2025-3-26 21:30 作者: 睨視 時(shí)間: 2025-3-27 02:47
https://doi.org/10.1007/978-1-349-24111-8be all parallel and continuous (i.e. long fibres). Thus each layer may be treated in a macroscopic sense as being a homogeneous, orthotropic material, for which the deformation behaviour is linearly elastic.作者: Rustproof 時(shí)間: 2025-3-27 08:16
https://doi.org/10.1007/979-8-8688-0369-7osites. Furthermore, associated hygrothermal expansion, either alone or in combination with mechanically induced deformation, can result in buckling, large deflections, and excessively high stress levels. Consequently, it is often imperative to consider environmental effects in the analysis and design of laminated systems.作者: 音樂(lè)學(xué)者 時(shí)間: 2025-3-27 10:30 作者: 改革運(yùn)動(dòng) 時(shí)間: 2025-3-27 15:41 作者: 小淡水魚(yú) 時(shí)間: 2025-3-27 21:48
Buckling and postbuckling theory for laminated composite platesbe all parallel and continuous (i.e. long fibres). Thus each layer may be treated in a macroscopic sense as being a homogeneous, orthotropic material, for which the deformation behaviour is linearly elastic.作者: 范例 時(shí)間: 2025-3-28 00:22 作者: 不合 時(shí)間: 2025-3-28 05:48 作者: 不容置疑 時(shí)間: 2025-3-28 08:05 作者: 種子 時(shí)間: 2025-3-28 12:39
Landschaften der Bundesrepublikociated) in their interior, in addition to at their exterior longitudinal edges, and that in some types of analysis the length of the strips which is considered for analysis purposes is less than the full length of the structure.作者: Meander 時(shí)間: 2025-3-28 16:01 作者: Progesterone 時(shí)間: 2025-3-28 20:20
Landschaften der Bundesrepublikr point supports); variable thickness; and with temperature-dependent material properties. The finite element method has enabled non-linear postbuckling analysis and sensitivity analysis, which can be used to study the sensitivity of the buckling and postbuckling responses to variations in the diffe作者: Guileless 時(shí)間: 2025-3-29 00:50
https://doi.org/10.1007/978-1-349-86035-7ia, certain new material imperfections can be found in composite structures in addition to the better-known imperfections that one finds in metallic structures. Thus, broken fibres, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute ma作者: 勛章 時(shí)間: 2025-3-29 04:58
https://doi.org/10.1007/978-1-349-86035-7tors include the use of discrete ply angles and layer thicknesses, restrained edges, shear deformation, cut-outs, thermal loading, strength and stiffness constraints, multiple design objectives and shape design.作者: 法律 時(shí)間: 2025-3-29 09:23
Finite element buckling and postbuckling analysesr point supports); variable thickness; and with temperature-dependent material properties. The finite element method has enabled non-linear postbuckling analysis and sensitivity analysis, which can be used to study the sensitivity of the buckling and postbuckling responses to variations in the diffe作者: 確定 時(shí)間: 2025-3-29 14:09
Delamination buckling of flat laminatesia, certain new material imperfections can be found in composite structures in addition to the better-known imperfections that one finds in metallic structures. Thus, broken fibres, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute ma作者: FANG 時(shí)間: 2025-3-29 17:11
Lay-up optimization of laminated plates under buckling loadstors include the use of discrete ply angles and layer thicknesses, restrained edges, shear deformation, cut-outs, thermal loading, strength and stiffness constraints, multiple design objectives and shape design.
