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The aim of this laboratory work is to design a strut/bracket assembly for aircrafts. Experiments are carried out to determine mechanical properties of certain materials.The material chosen is Mild Steel. Given the possible condition experienced by the material and the safety factor, the dimensions for the designs of the strut/bracket assembly for aircrafts are obtained to avoid failure by yield or fracture. The diameter of the pin, d ,which is subjected to shear stress should be larger than 14.56mm. The diameter of the rod, D, should be larger than 12.74mm. The thickness of the rod would be 10mm.
An example showing how to use BibTeX to manage your bibliography.
This example was originally published on ShareLaTeX and subsequently moved to Overleaf in November 2019.
Important Note: This template is no longer supported, but is provided for historical reference.
This template for Wiley article submissions was developed by Overleaf for the Overleaf-Wiley pilot which ran during 2017 and 2018. It was last updated in January 2019.
If you're planning to submit to a Wiley journal, please check the journal's author guidelines page for the latest information on how to prepare your submission.
Wiley and Overleaf
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