合金主成份對航空用7050鋁合金之影響研
碩士 === 國立中央大學 === 機械工程研究所 === 86 === This study was to research the effect of main alloy content (Zn and Mg) on the strength and elongation in order to clatify the relation between heat treatment and the strength of 7050 aluminum alloy for aerospace. Controlling microstructure was simultaneously...
Main Author: | 陳永豪 |
---|---|
Other Authors: | 歐炳隆 |
Format: | Others |
Language: | zh-TW |
Published: |
1998
|
Online Access: | http://ndltd.ncl.edu.tw/handle/77412535985524449241 |
Similar Items
-
航空用鋁合金之超塑性評估
by: PU,HAN-PING, et al.
Published: (1991) -
合金成份與熱處理製程對6063鋁合金擠型性及機械性質影響之研究
by: Young-Houng Fan, et al.
Published: (1999) -
高強度、高抗應力腐蝕破壞性7050鋁合金合金設計之研究
by: Ho-Wen Chen, et al.
Published: (1999) -
高中生人生觀之主成份分析
by: 林永宗
Published: (2009) -
主成份迴歸中主成份選擇法之建立與比較-均方誤矩陣VSPITMAN
by: 蔡秒玉
Published: (2001)