ASTM F3601-23

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1.1 This practice provides guidance for verification and validation of structural finite element models (FEMs) that are used to support showings of compliance with Civil Aviation Authority (CAA) regulations. This encompasses FEM predictions of internal loads, displacements, strains, stresses, stability, and post-buckling loads.

Product Details

Published:
03/01/2023
Number of Pages:
4
File Size:
1 file , 260 KB
Note:
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