Hello to all,
This an attempt to calculate a fuselage truss. It's isostatic and concern the end cone frame from cabane to fuselage end.
Let me tell if it's a solution or not, I did it 2 years ago and left as it is; But I have another truss project and would like to know if I'm right or wrong.
It's a GoogleSheet that address is at
google sheet truss calculus
Thanks for your answers and remarks: Here it is inserted in the post to give you a glimpse of it but you should have a better rendering with link above and see formulas used in cells
This an attempt to calculate a fuselage truss. It's isostatic and concern the end cone frame from cabane to fuselage end.
Let me tell if it's a solution or not, I did it 2 years ago and left as it is; But I have another truss project and would like to know if I'm right or wrong.
It's a GoogleSheet that address is at
google sheet truss calculus
Thanks for your answers and remarks: Here it is inserted in the post to give you a glimpse of it but you should have a better rendering with link above and see formulas used in cells
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