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A310 Fuselage Cross Section to find Inertia and Centroid Values

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sb1786

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Oct 7, 2008
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Hello All,

I am trying to find the bending stress at an antenna location. The fromula is stress = Moment*centroid/Inertia.

I am having a lot of trouble finding a model or data to model a cross section of the fuselage at location staion 2163. This would help me find the inertia and centroid values I am after.

Anyone knows how I can go about with this. Any tips, help, previous experience?

Thanks
 
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thanks taglia.
Maybe i can set up an ftp for you where you can upload it. How big is it?

Anyone know howcome RAPID is not offered and supported by the FAA anymore?
 
taglia,

i was able to dowload from the link provided but u only put the application file rapid.exe.

i need the installer.

Thanks
 
Don´t know what happpens, I couldn´t post the installer, the uploading is interrupted even whith Rapidshare. I´m sorry. I hope you can do it with the other address you mention.
 
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