| 发明名称 |
COMBINED LOADING IN COMPOSITE MATERIALS |
| 摘要 |
A method for determining material failure that includes the steps of: fabricating a coupon made of a material; applying first force and second forces on the coupon, where the second force is different than the first force; and characterizing a material failure due to the application of the first force and the second force to the coupon. |
| 申请公布号 |
US2016139016(A1) |
申请公布日期 |
2016.05.19 |
| 申请号 |
US201414547844 |
申请日期 |
2014.11.19 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
Kismarton Max U.;Cregger Samuel Eric |
| 分类号 |
G01N3/08;G06F17/50 |
主分类号 |
G01N3/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for determining material failure, comprising the steps of:
fabricating a coupon made of a material; applying a first force on the coupon; applying a second force on the coupon, wherein the second force is different than the first force; and characterizing a material failure due to the application of the first force and the second force. |
| 地址 |
Chicago IL US |
