Aerospace_lug_analysis.xls

This method of assessment involves reading coefficients from graphical data for use in subsequent equations. The spreadsheet automates all the curve reading to determine the proof and ultimate strength of lugs in an expedient manner. The spreadsheet has been produced by Abbott Aerospace an independent consultancy company offering structural engineering services the aerospace industry. You can contact them by email This e-mail address is being protected from spam bots, you need JavaScript enabled to view it

abbottaerospace

 Laminate_Stress_Strain_Analysis.xls  New!

The User input cells are light blue background with bold dark blue text.
The thickness column over rides the material lamina thicknesses - for use with core materials
The Strain approach includes damage effects, the stress approach does not
Any comments or error reports are appreciated
Notes:
The Biaxial strain envelope is typically conservative for biaxial compression
The Mohr's circle approach is typically conservative for shear
The interacted margin of safety is for the Mohr's circle method
All material data is typical - may not be accurate

The spreadsheet has been produced by Abbott Aerospace an independent consultancy company offering structural engineering services the aerospace industry. You can contact them by email This e-mail address is being protected from spam bots, you need JavaScript enabled to view it

abbottaerospace