1) time interval of advancement
推进的时间间隔
3) time advance
时间推进
1.
Time management is an important component of High Level Architecture,in the simulation system that based on HLA,any federation member s deadlock in the time advance process can lead the whole federation can not be able to advance any more.
时间管理服务是高层体系结构HLA(High Level Architecture)的重要组成部分,在基于HLA的仿真系统中,联邦成员在时间推进过程中产生的死锁往往会导致整个系统仿真无法向前推进。
2.
This paper mainly introduces the time management policy and time advance method provided by RTI,basing on the production of basic time management notion.
在介绍时间管理相关概念的基础上,重点讨论高层体系结构(HLA)中联邦成员RTI所提供的时间管理策略及时间推进方法。
4) time advancing
时间推进
1.
The mechanism of time advancing in the mode of TDMA is analyzed.
以新一代分布式交互仿真体系结构HLA为基础,结合RTI软总线的功能,详细分析了TDMA无线通讯方式下时间推进机制和信息发送的实现。
5) explicit time marching method
时间推进法
1.
According to the theory of the multi-grid scheme,this paper puts forward a new multiple-grid scheme in the calculation of the diffuser grid flow field of NASA67,which is used with the combination of explicit time marching method,finite volume difference code and distributed body force.
根据在流场数值计算中使用多重网格方法可以加速收敛的原理,在叶栅流场控制方程使用有限体积差分法进行离散的前提下,提出了一种新的4重网格方法来加速求解压气机叶栅可压缩流动,该方法可以与显式时间推进法有效配合使用。
6) time marching method
时间推进法
1.
In this paper the incompressible Reynolds-averaged Navier-Stokes equations for the centrifugal pump were solved by using of time marching method.
本文使用时间推进法求解离心泵内部不可压缩流的紊流时均Reynolds方程。
2.
The time marching method was used to solve the control equations, and a computational analysis of the flow field in a centrifugal compressor with unshrouded impeller and vaned diffuser was presented.
应用时间推进法求解连续性方程、时均N-S方程、能量方程、理想气体状态方程及Yang＆Shihk-ε紊流模型,对含分流叶片的半开式叶轮及叶片扩压器组成的离心压缩机模型级级内三维粘性流场进行了数值分析,得出了与实测结果一致的性能曲线。
3.
This paper puts forward a new multiple gird scheme, which is used with the combination of explicit time marching method, finite volume difference code and distributed body force.
本文提出了一种新的多重网格法 ,并将之与显式时间推进法、有限体积差分格式、粘性体积力法配合使用求解离心压气机内部流场。
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条