Abstract
In order to study isothermal forming rules of aerospace aluminum alloy forgings, we have simulated the forming process of different billet shapes, and compared the deformation mechanism and load characteristics. Comparing experimental and theoretical values of both sides of wall thickness shows that the maximum error is only 3.4% meeting the specification requirements.
| Original language | English |
|---|---|
| Pages (from-to) | 62-65 |
| Number of pages | 4 |
| Journal | JOM |
| Volume | 63 |
| Issue number | 11 |
| DOIs | |
| State | Published - Nov 2011 |
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