该文介绍了大型下沉式盾构掘进机综合模拟试验平台的总体设计。
The article introduces the overall design of integrate simulating experimental platform of large-sized sunk shield tunneling machine.
采用总体空气动力学边界层及显式水汽方案的控制试验较成功地模拟出了气旋涡度场的型式和中心强度。
Both the pattern and central intensity of the vorticity field have been simulated successfully using the bulk aerodynamic boundary layer and apparent vapor scheme in the model.
通过模拟试验分析该协议，表明其能有效地减少重要性大事务的失效率，但对总体事务的失效率影响不大。
Experiment results show that the new protocol can effectively reduce miss -ratio of transaction with greater importance while influencing the overall miss-ratio slightly.
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