| Process Induced Residual Stress and Deformation in a Ring-Stiffened Composite Launching Tube |
| 關(guān)鍵詞： |
filament winding. |
| 類(lèi) 別： |
復(fù)合材料 >> 樹(shù)脂基復(fù)合材料 |
| 來(lái) 源： |
2009年第四屆中歐增強(qiáng)高聚物工藝與性能?chē)?guó)際學(xué)術(shù)會(huì)議（桂林，June 8-12) |
| 資料類(lèi)型： |
pdf文件 |
| 資料大小： |
170K |
| 簡(jiǎn) 介： |
Composite materials are being used to fabricate launching tubes for strategic missiles
due to their excellent specific strength and stiffness over traditional metal materials.
The favoured method of manufacture is filament winding. Depending on lay-up and
cure cycle, large localized residual stresses can be generated during processing which
could cause defects such as layer separation, micro-cracking and poor dimensional fidelity. |
| 上傳人： |
magicpower |
| 上傳時(shí)間： |
2009-08-05 10:21:53 |
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