航天發動機噴嘴機構建模

本篇文章以航天發動機為例,介紹了基于samcef mecano計算平臺的實例仿真。對發動機噴嘴進行了三維建模及有限元仿真。

題目為:3D Kinematics Studywith SAMCEF MECANO Motion on a nozzle of a turbojet engine - Pre andpost-processing in SAMCEF Field




this paper presents different ways to simulate a jet engine nozzle motion. The case helps to validate the use of the new software SAMCEF Field & SAMCEF Mecano/Motion on complex nozzle mechanism. It also gives an overview of potential areas of interest for the design of future systems. After a quick sum-up of engine nozzle design philosophy, we will detail the various phases to define the mechanism model, from use of CAD model to detailed analysis.



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