派博傳思國際中心

標題: Titlebook: Composite Structures 4; Volume 1 Analysis an I. H. Marshall Book 1987 Elsevier Applied Science Publishers Ltd 1987 composite material.defor [打印本頁]

作者: Cataplexy    時間: 2025-3-21 18:40
書目名稱Composite Structures 4影響因子(影響力)




書目名稱Composite Structures 4影響因子(影響力)學(xué)科排名




書目名稱Composite Structures 4網(wǎng)絡(luò)公開度




書目名稱Composite Structures 4網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Composite Structures 4被引頻次




書目名稱Composite Structures 4被引頻次學(xué)科排名




書目名稱Composite Structures 4年度引用




書目名稱Composite Structures 4年度引用學(xué)科排名




書目名稱Composite Structures 4讀者反饋




書目名稱Composite Structures 4讀者反饋學(xué)科排名





作者: legislate    時間: 2025-3-21 22:22
Stability of an Orthotropic Plate Subjected to a Follower Forcening differential equation derived by Brunelle and Oyibs in affine space is used. The Levy-type solution method is used to solve the vibration problems. The optimization package ADS is employed to find the dynamic stability loading. The effect of generalized rigidity ratio D* on the stability boundaries is presented.
作者: 生意行為    時間: 2025-3-22 00:28

作者: Biguanides    時間: 2025-3-22 05:16

作者: 運動性    時間: 2025-3-22 12:11
Grundlagen und Ziele statistischer Methoden,l applications of joints into consideration. In bearing failure modes the creep life is shorter than the time of the final failure, which is confirmed in the low and high cycle fatigue tests. The creep life of hybrid constitutions can be predicted by applying the law of mixtures.
作者: FUME    時間: 2025-3-22 16:17

作者: FUME    時間: 2025-3-22 17:21

作者: 出來    時間: 2025-3-22 22:27

作者: 戲法    時間: 2025-3-23 05:00
Wind Turbines—The Potential for CompositesThe paper provides an overview of the emerging wind turbine industry particularly in the UK. It explores the potential for introducing composite materials into a whole range of components which are obtained in wind turbines and why traditional materials solutions can be the source of problems.
作者: 手術(shù)刀    時間: 2025-3-23 09:03

作者: Small-Intestine    時間: 2025-3-23 13:23
Grundlagen und Ziele statistischer Methoden, low-powered ground terminals will demand improved space craft radio frequency performance which will lead in turn to the use of large antennas..A number of space missions have been proposed incorporating reflectors of very large diameter. These applications include mobile satellite systems, broadca
作者: eardrum    時間: 2025-3-23 16:31
https://doi.org/10.1007/978-3-662-22684-1fied for application to thin platforms, and a mathematical model is constructed for predicting outgassing rates as a function of orbital temperatures. It is found that small changes in temperature can have a major influence on the time needed for a structure to reach a specified level of residual co
作者: Generic-Drug    時間: 2025-3-23 18:43

作者: 笨拙處理    時間: 2025-3-24 00:49
Grundlagen und Ziele statistischer Methoden,l applications of joints into consideration. In bearing failure modes the creep life is shorter than the time of the final failure, which is confirmed in the low and high cycle fatigue tests. The creep life of hybrid constitutions can be predicted by applying the law of mixtures.
作者: 拱形面包    時間: 2025-3-24 02:30
https://doi.org/10.1007/978-3-642-96504-3mbled without protrusions. The inserts consist of two mating surfaces which interlock through the existence of a shoulder male boss and a shoulder female counterbore. Repeated assembly and disassembly can take place without damaging the material being fastened. The strength of the joint, when using
作者: objection    時間: 2025-3-24 09:41
,Wieviel Beobachtungen werden ben?tigt?,ning differential equation derived by Brunelle and Oyibs in affine space is used. The Levy-type solution method is used to solve the vibration problems. The optimization package ADS is employed to find the dynamic stability loading. The effect of generalized rigidity ratio D* on the stability bounda
作者: Neolithic    時間: 2025-3-24 12:46

作者: FATAL    時間: 2025-3-24 18:31
,Wieviel Beobachtungen werden ben?tigt?,t-section stiffeners. Particular reference is made to the effects of interaction between local buckling of the panel laminate and overall column-like buckling involving bending of the stiffeners. Conclusions are reached regarding the influence of interactive effects on collapse strength and recommen
作者: 玉米棒子    時間: 2025-3-24 22:35

作者: 完成才能戰(zhàn)勝    時間: 2025-3-24 23:25
Helmut Günzler,A. M. Bahadir,H. Wissermaterials. The classical plate theory, which accounts for the bimodular action and large rotations, is employed. Finite element results for transverse deflection are presented for simply-supported, graphite/epoxy and polyester-rubber plates under uniform distributed load. Also, the effects of the as
作者: escalate    時間: 2025-3-25 04:12

作者: Nonthreatening    時間: 2025-3-25 09:32
Die Sch?tzung von Verh?ltniszahlenbox is presented. The design features incorporated have been proven in the author’s testing programme. This is leading to the testing of a full-scale wing box for an aerobatic light aircraft. Various means of improving the strength of skin/stiffener junctions are described, including the use of Kevl
作者: 同謀    時間: 2025-3-25 13:58
Zur Planung von Projekten: Rechtzeitig zu Bly discusses structural design of 32-m diameter GRP/composite blade for 200-kW wind turbine. Description of the main formulae of aerodynamic loads and centrifugal forces is given. The strength and stiffness of the GRP/composite blade can be calculated and tailored according to the load characteristi
作者: innate    時間: 2025-3-25 16:47
Einführung und sechs übersichtenis the ability to manufacture the rotor blades at low cost in a configuration which will meet the severe structural requirements, produce a high level of performance and have a long life with low maintenance. A new manufacturing method has been conceived and successfully tested..Details on the proce
作者: DAFT    時間: 2025-3-25 23:02
https://doi.org/10.1007/978-3-642-95169-5e rate of use has increased progressively as confidence in the material and the process has been gained. In this chapter the mechanical and structural performance is discussed based on short-term and long-term testing of the actual pipe. The results of the short-term testing include burst pressure,
作者: ASSET    時間: 2025-3-26 04:05

作者: 擺動    時間: 2025-3-26 05:40
Spezielle diskrete Verteilungenthe circular ring cut from them. Two modification factors must be regarded. The first one results from the additional bending stress in the region near the mid-plane. Two new mechanical models are suggested for calculating the bending stress mentioned above. The second factor is the influence of the
作者: moratorium    時間: 2025-3-26 10:00

作者: Foment    時間: 2025-3-26 16:16
A Composite Structural System for a Large Collapsible Space Antenna low-powered ground terminals will demand improved space craft radio frequency performance which will lead in turn to the use of large antennas..A number of space missions have been proposed incorporating reflectors of very large diameter. These applications include mobile satellite systems, broadca
作者: 異常    時間: 2025-3-26 16:59
Outgassing of Spacecraft Compositesfied for application to thin platforms, and a mathematical model is constructed for predicting outgassing rates as a function of orbital temperatures. It is found that small changes in temperature can have a major influence on the time needed for a structure to reach a specified level of residual co
作者: Commonplace    時間: 2025-3-26 23:17

作者: 原諒    時間: 2025-3-27 03:12

作者: Phenothiazines    時間: 2025-3-27 07:36
Inserts for Fastening Sheet Molding Compoundsmbled without protrusions. The inserts consist of two mating surfaces which interlock through the existence of a shoulder male boss and a shoulder female counterbore. Repeated assembly and disassembly can take place without damaging the material being fastened. The strength of the joint, when using
作者: 鈍劍    時間: 2025-3-27 13:10

作者: larder    時間: 2025-3-27 16:44

作者: 截斷    時間: 2025-3-27 18:08

作者: PHONE    時間: 2025-3-27 22:00

作者: 有權(quán)    時間: 2025-3-28 04:03

作者: insolence    時間: 2025-3-28 10:05

作者: ingestion    時間: 2025-3-28 13:17

作者: Pseudoephedrine    時間: 2025-3-28 16:35

作者: 作嘔    時間: 2025-3-28 21:15
Design, Manufacturing and Tests of Large Wind Turbine Rotor Bladesis the ability to manufacture the rotor blades at low cost in a configuration which will meet the severe structural requirements, produce a high level of performance and have a long life with low maintenance. A new manufacturing method has been conceived and successfully tested..Details on the proce
作者: Preserve    時間: 2025-3-29 01:05
Structural Performance of Centrifugally Cast Glass Reinforced Plastic Pipese rate of use has increased progressively as confidence in the material and the process has been gained. In this chapter the mechanical and structural performance is discussed based on short-term and long-term testing of the actual pipe. The results of the short-term testing include burst pressure,
作者: 為寵愛    時間: 2025-3-29 07:04
The Support of Horizontal Cylindrical GRP Vessels—Saddles or Longitudinal Beams?examine the way in which these supports influence the strain distribution in the vessel, results are presented from a series of experimental investigations. These have been carried out on a 1 m diameter, 4 m long, CSM reinforced polyester vessel subject to hydraulic loading. In the first series of t
作者: 全部逛商店    時間: 2025-3-29 09:28

作者: 怎樣才咆哮    時間: 2025-3-29 11:54
f Technology, Scotland in July 1987. The Conference was organised and sponsored by Paisley College of Technology. It was co-sponsored by the Scottish Development Agency, the National Engineering Laboratory, the US Air Force European Office of Aerospace Research and Development and the US Army Resear
作者: patella    時間: 2025-3-29 17:10
https://doi.org/10.1007/978-3-662-22684-1 It is found that small changes in temperature can have a major influence on the time needed for a structure to reach a specified level of residual contamination. Numerical examples are presented to illustrate application of the theory, and recommendations are given for testing and for monitoring orbital temperatures.
作者: plasma-cells    時間: 2025-3-29 21:30

作者: single    時間: 2025-3-30 00:37

作者: 流浪者    時間: 2025-3-30 05:13

作者: Laconic    時間: 2025-3-30 11:25
Einführung und sechs übersichten of performance and have a long life with low maintenance. A new manufacturing method has been conceived and successfully tested..Details on the process and the ongoing qualification program are given.
作者: 財主    時間: 2025-3-30 15:52

作者: 闡釋    時間: 2025-3-30 20:33
Interactive Buckling Effects in Stiffened FRP Panelsbuckling involving bending of the stiffeners. Conclusions are reached regarding the influence of interactive effects on collapse strength and recommendations are made on allowance for these effects in design.
作者: 依法逮捕    時間: 2025-3-31 00:34

作者: Mobile    時間: 2025-3-31 03:49
Design of the ARALL F-27 Lower Wing Fatigue Paneling of the Fokker F-27 Friendship has been selected as a design study for this purpose. In this chapter the design philosophy and detail design, as well as results of the finite element analyses and CAD procedures will be presented. Also the preliminary fatigue test results will be discussed briefly.
作者: 意外    時間: 2025-3-31 08:37

作者: 杠桿支點    時間: 2025-3-31 11:02
https://doi.org/10.1007/978-3-0348-4167-2her materials, local effects, nonlinear stress-strain relationships, and hygrothermal effects. Postbuckling behavior and the effects of initial geometric imperfections are also discussed. The results summarized are taken from a recent comprehensive study of the world’s literature on this subject, encompassing approximately 300 references.
作者: BOGUS    時間: 2025-3-31 16:46
https://doi.org/10.1007/978-3-642-96504-3me is also investigated. The difference between the dry and wet strengths for the inserted samples is less than that for the bolted samples. Load versus extension plots show that these particular inserts provide a more rigid joint than a bolted connection.
作者: 領(lǐng)先    時間: 2025-3-31 21:08
Zur Planung von Projekten: Rechtzeitig zu Bue is serious in large blades, we calculate the structural response by using Friedmann’s aeroelastic modelling..Blades are a key part of a rotor and their performances have a great influence on the performances of the rotor machine. GRP/composite will be very satisfactory for the aerodynamic and structural requirements of the blade.
作者: Vital-Signs    時間: 2025-4-1 00:44
An Overview of Composite Plate Bucklingher materials, local effects, nonlinear stress-strain relationships, and hygrothermal effects. Postbuckling behavior and the effects of initial geometric imperfections are also discussed. The results summarized are taken from a recent comprehensive study of the world’s literature on this subject, encompassing approximately 300 references.
作者: 后天習(xí)得    時間: 2025-4-1 04:36
Inserts for Fastening Sheet Molding Compoundsme is also investigated. The difference between the dry and wet strengths for the inserted samples is less than that for the bolted samples. Load versus extension plots show that these particular inserts provide a more rigid joint than a bolted connection.
作者: 分離    時間: 2025-4-1 08:35





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