Using 3-D rigid-viscoplastic finite element method, the multi-stage forging process of a gas turbine compressor blade was simulated.

 
  • 利用剛粘塑性有限元法,對某重型燃機壓氣機葉片的多工步鍛造過(guò)程進(jìn)行了三維有限元模擬。
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