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流体网络节点残量修正算法的改进 被引量:2

Improvement of Fluid Network Node Residue Correction Algorithm
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摘要 为了提高流体网络求解的收敛性与稳定性,对网络节点残量修正算法进行改进。基于理论分析,提出使残量修正算法大范围收敛的初值赋值规律,并通过简单模型的数值分析加以验证;在节点残量修正显式迭代的基础上,提出隐式梯形迭代格式,扩大最大迭代步长。基于改进方法,以某典型航空发动机空气系统为例进行计算,获得空气系统各节点的压力、温度以及各支路的质量流量。该计算过程显示,相对于残量修正显式迭代,改进计算振荡大幅度减弱,收敛速度提高了80%以上。结果表明:改进算法有效地提高了流体网络求解的稳定性和收敛性。 In order to enhance stability and convergence of solving fluid network, the network node residue cor- rection algorithm is investigated. Based on theory analysis, a principle of setting initial values for network is put forward which enables the algorithm to converge in large scale. Implicit trapezoid iteration formula is advanced on the foundation of node residue correction explicit expression, making maximum iterative step expand a lot. One certain aero engine secondary air system is computed with the improved algorithm above as an example, whose pressure distribution, temperature distribution and mass f^ow distribution are obtained. The computation process shows that calculation oscillation is greatly reduced and convergence speed is improved by more than 80% compared with the explicit iteration. It indicates that the improved algorithm ameliorates stability and con- vergence of solving fluid networks effectively.
出处 《航空工程进展》 2012年第3期274-278,共5页 Advances in Aeronautical Science and Engineering
基金 西北工业大学科技创新基金(2009kj010006)
关键词 流体网络 节点残量修正 收敛性和稳定性 赋值规律 隐式梯形迭代 fluid network node residue correction convergence and stability principle of setting initial values implicit trapezoid iteration
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  • 1<航空发动机设计手册>总编委会.航空发动机设计手册[M]北京:航空工业出版社,2001.
  • 2Majumdar A K,Bailey J W,Schallhorn P. A generalized fluid system simulation program to model flow distribution in fluid networks.NASA-CR 207793[R].1998.
  • 3Muller Y. Secondary air system model for integrated thermomechanical analysis of a jet engine.ASME-GT 50078[R].2008.
  • 4Alexiou A,Mathioudakis K. Secondary air system component modeling for engine performance simulations[J].Journal of Engineering for Gas Turbines and Power,Transactions of the ASME,2009,(03).
  • 5Kutz K J,Speer T M. Simulation of the secondary air system of aero engines[J].Journal of Turbomachinery,Transactions of the ASME,1994,(02):306-315.
  • 6Van Hooser K,Bailey J,Majumdar A. Numerical prediction of transient axial thrust and internal flows in a rocket engine turbopump.AIAA-99-2189[R].1999.
  • 7吴丁毅.内流系统的网络计算法[J].航空学报,1996,17(6):653-657. 被引量:40
  • 8吕亚国,刘振侠,黄生勤.航空发动机内流空气系统通用分析软件设计[J].计算机仿真,2009,26(7):99-103. 被引量:12
  • 9欧阳洁;聂玉峰;车刚明.数值分析[M]北京:高等教育出版社,2009.
  • 10王新月.气体动力学基础[M]西安:西北工业大学出版社,2006.

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