版權說明:本文檔由用戶提供并上傳,收益歸屬內(nèi)容提供方,若內(nèi)容存在侵權,請進行舉報或認領
文檔簡介
1、南京航空航天大學碩士學位論文鋁蜂窩夾層板的力學性能等效模型研究姓名:趙金森申請學位級別:碩士專業(yè):工程力學指導教師:鄧宗白20061201鋁蜂窩夾層板的力學性能等效模型研究 IIABSTRACT As a kind of special compound materials, The aluminum honeycomb sandwich structures have been widely used in the fields of
2、 spaceflight, aviation and ships etc, because of superior of material function .In various forms of aluminum honeycomb core, aluminum honeycomb core of positive hexagon is applied most extensively .To improve product qua
3、lity and use safely and dependably, the research on its mechanical function is very necessary .Currently during the analysis of finite element method software of international popularity and authorization don’t have stan
4、dard honeycomb sandwich element. This text did a lot of research on structure of the core ,macroscopic mechanical function of honeycomb sandwich plates ,experiments and so on ,with honeycomb core of positive hexagon main
5、 research object. From the deficiency the of the front scholar’s research on positive hexagon core, the paper presented the Y mode, then carried the research on the honeycomb core according to the Y model, and deduced th
6、e mechanical parameters for the core by the mechanical analysis; even used the energy method to study mechanical parameters of positive hexagon core first time; lastly did computer simulation of parts of mechanical param
7、eters. The thesis presented current research results. It improved the three point bending by the principle of equality to each other of work, and deduced the method of testing bending stiffness and shearing stiffness of
8、aluminum honeycomb sandwich plates. Then some experiments were done, and the results of experiment were identical to academic result. The thesis presented the current equivalent models of aluminum honeycomb sandwich plat
9、es. They are static equivalent, dynamic equivalent, and the sandwich theories .Then it revised Allen’s method by considering to bending stiffness of core, and gave the engineering calculation method, it also used the glu
10、ed beam model to compute the aluminum honeycomb sandwich plates .In the end it computed the concrete examples. In contact with the request of dynamics for studying to the structural inherent frequency, the paper gave the
11、 formulae of aluminum honeycomb sandwich plates under simply supported; and computed the examples of chapter 4 by using ANSYS software and academic formulae. It pointed out that which methods applied, which methods were
溫馨提示
- 1. 本站所有資源如無特殊說明,都需要本地電腦安裝OFFICE2007和PDF閱讀器。圖紙軟件為CAD,CAXA,PROE,UG,SolidWorks等.壓縮文件請下載最新的WinRAR軟件解壓。
- 2. 本站的文檔不包含任何第三方提供的附件圖紙等,如果需要附件,請聯(lián)系上傳者。文件的所有權益歸上傳用戶所有。
- 3. 本站RAR壓縮包中若帶圖紙,網(wǎng)頁內(nèi)容里面會有圖紙預覽,若沒有圖紙預覽就沒有圖紙。
- 4. 未經(jīng)權益所有人同意不得將文件中的內(nèi)容挪作商業(yè)或盈利用途。
- 5. 眾賞文庫僅提供信息存儲空間,僅對用戶上傳內(nèi)容的表現(xiàn)方式做保護處理,對用戶上傳分享的文檔內(nèi)容本身不做任何修改或編輯,并不能對任何下載內(nèi)容負責。
- 6. 下載文件中如有侵權或不適當內(nèi)容,請與我們聯(lián)系,我們立即糾正。
- 7. 本站不保證下載資源的準確性、安全性和完整性, 同時也不承擔用戶因使用這些下載資源對自己和他人造成任何形式的傷害或損失。
最新文檔
- 鋁蜂窩夾層板等效模型研究及數(shù)值分析.pdf
- 含缺陷蜂窩夾層板的彎曲力學性能分析.pdf
- 釬焊鋁蜂窩板的研制與力學性能研究.pdf
- 矩形填充多孔材料夾層結構的力學性能等效模型研究.pdf
- 泡沫鋁芯體夾層板的動態(tài)力學性能研究.pdf
- 蜂窩夾層微帶天線力學性能研究.pdf
- 金屬蜂窩夾層結構的力學性能分析.pdf
- 帶缺陷蜂窩夾層結構的力學性能實驗研究.pdf
- 蜂窩鋁夾芯板的剪切、壓縮力學性能研究.pdf
- 鋁蜂窩夾層板耦合損耗因子研究.pdf
- 鋁基復合材料夾層板與填充圓管力學性能研究.pdf
- 紙基復合蜂窩板力學性能研究.pdf
- 蜂窩夾層橡膠支座力學性能的理論分析與試驗研究.pdf
- 玄武巖纖維增強泡沫鋁夾層板的制備與力學性能研究.pdf
- 輕木夾層板力學性能分析.pdf
- 金屬熱防護結構蜂窩板力學性能研究.pdf
- 鎂合金蜂窩板的制備及力學性能研究.pdf
- 復合材料蜂窩夾層結構制備及其力學性能分析.pdf
- 含缺陷復合材料蜂窩夾層結構力學性能研究.pdf
- 鋁蜂窩夾層板的統(tǒng)計能量參數(shù)辨識.pdf
評論
0/150
提交評論