Abstract
This paper is about the analysis and design of avionics equipment`s housing and PCB(Printed Circuit Board) such as air data computer. Avionics equipment`s structural design as well as electrical properties is very critical and should be proved from design phase by analysis method. First, analyze the static load and vibration requirement for the installed equipment, and then proved it satisfy with its requirement using the computational structural analysis. Commercial tools were used for computation and the rib design of housing was verified and the placement of electrical component was proposed using the PCB`s local displacement information.
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