The Institute of Theoretical and Applied Mechanics 2 records found  Search took 0.05 seconds. 
1.
It is common for Finite Element Model (FEM) validation activities to be carried out in the modal domain; using finite element modal analysis results and modal parameters [...]
2.
The vibrations that a spacecraft experiences during launch are critical for the safety and integrity of its payload. To simulate the launch, a Coupled Load Analysis (CLA) [...]

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