[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.
| Google drive docs |
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| url | https://docs.google.com/document/d/1myumzEO4m2dKqoKbSpjWJIvn293NRYBAp9Xgpa-KLLc/edit?usp=sharing |
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| Google drive sheets |
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url | https://docs.google.com/spreadsheets/d/1QQbEP5SHA8hwQXX6dZYUG9Nn7Oq-_HDE0FsRvXqO4Rg/edit#gid=16511098This thread of pages will be dedicated to organizing the research and calculations related to this project.