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Large double curvature panels are widely used in manufacture of modern aircraft bodies. One of the possible ways to manufacture such parts is to form a workpiece using the method of high temperature multi-point forming by means of a set of moving cores. The paper considers workpiece forming process using different core unit configurations and presents the results of workpiece behaviour study during forming, obtained by means of a finite element method. Conclusions are made on the existing interconnections between forming cores during the forming process.

Studying Interaction of Multi-Motor Forming System for Double Curvature Items