Research on High Aspect Ratio Aircraft Load Design Envelops Using Structural Stress Selecting Method
The load design condition of structure strength computation must be selected due to the limited technique condition and aircraft development time, so it is necessary to study the envelopes of total load for structure component and simplified engineering girder load distribution. The load envelope me...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2020-10-01
|
| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019135?st=article_issue |