The transonic flow field around NACA 0012 airfoil is calculated by finite element method from pressure minimum integration, full potential equation being used.
本文采用压强极小积分有限元法计算了NACA 0012翼型的跨音速流场。出发方程为全速位方程。
From these diverse capabilities, I defined the minimum capabilities to establish an ESB as providing for communication, integration, and service interactions.
从这些不同的功能中，我确定了建立ESB所需的最低功能，包括通信、集成和服务交互。
The integration effort needs to be carefully planned and coordinated so that changes can be kept to a minimum.
集成方面的工作需要详细计划和协调，以使变化被保持在最小。
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