[Work in Progress]
The integration between the aerobody panels and the chassis will be through the application of structural adhesives at interfacing areas. The following are calculations and research related to adhesive requirements.This thread of pages will be dedicated to organizing the research and calculations related to this project.
Current Docs Used for Research:
| Google drive docs |
|---|
| url | https://docs.google.com/document/d/1myumzEO4m2dKqoKbSpjWJIvn293NRYBAp9Xgpa-KLLc/edit?usp=sharing |
|---|
|
| Google drive sheets |
|---|
| url | https://docs.google.com/spreadsheets/d/1QQbEP5SHA8hwQXX6dZYUG9Nn7Oq-_HDE0FsRvXqO4Rg/edit#gid=16511098 |
|---|
|