期刊文献+

频散可控格式的一种推广形式及其在爆轰波马赫反射中应用 被引量:3

A General Form of the Dispersion-controlled Dissipative Scheme and Its Application in Detonation Problems
下载PDF
导出
摘要  频散可控格式是高精度捕捉激波的新格式.对原有频散可控格式(DCD)进行了推广,给出了适用于网格点排列不规则情况下的DCD格式,使其具有更广泛的适应性,在此基础上构造了在非结构三角形网格下的DCD格式.用一些典型算例对推广后的DCD格式进行检验,结果表明该格式是合理和可靠的,并能够较好地保留原有DCD格式的二阶精度.把推广后的DCD格式和具有8种组分和20个化学反应的基元反应模型相结合,对氢氧爆轰波在直管道中的传播问题及楔面上马赫反射问题进行计算,计算结果和实验结果比较表明,在非结构三角形网格下的DCD格式能够有效地捕捉爆轰波,在爆轰波阵面上不会产生振荡或是抹平间断现象. A general form of the dispersion-controlled dissipative(DCD)scheme is proposed.An unstructured DCD is constructed and its reliability is demonstrated with numerical simulations.Comparisons of the unstructured results with the second order structured results reveal that the previous resolution is well retained.In order to simulate detonation problems,unstructured DCD is combined with detailed chemical reaction kinetics.The algorithm is used to simulate detonation propagating along a straight duct with or without a wedge.Comparison of the numerical simulations and experiments shows that the algorithm works well in capturing detonation waves.Neither numerical oscillation nor artificial viscosity occurs in practical calculations.
出处 《计算物理》 CSCD 北大核心 2005年第3期189-196,共8页 Chinese Journal of Computational Physics
基金 国家自然科学基金 中国工程物理研究院(NASF10276035)资助项目
  • 相关文献

参考文献2

二级参考文献2

共引文献15

同被引文献15

  • 1王丁喜,严传俊.脉冲爆震发动机进气道气动性能的数值研究[J].力学学报,2005,37(6):777-782. 被引量:6
  • 2常利娜,姜宗林.球面聚心气相爆轰波传播过程的数值研究[J].力学学报,2006,38(3):296-301. 被引量:2
  • 3Terao K,Akaba H,Shiraishi H.Spherically imploding detonation waves initiated by a two-step divergent detonation.Shock Waves,1995,4:187-193 被引量:1
  • 4Barenblatt GI,Zeldovich Ya B.Self-similar solutions as intermediate asymptotics.Annu Rev Fluid Mech,1972,4:285-312 被引量:1
  • 5Guderley G.Powerful spherical and cylindrical compression shocks in the neighborhood of the center of the sphere and of the cylinder axis.Luftfahrtforsch,1942,19:302-312 被引量:1
  • 6Bonnie J.McBride,Michael J.Zehe,Sanford Gordon.NASA Glenn Coefficients for Calculating Thermodynamic Properties ofIndividual Species,National Aeronautics and Space Administration Glenn Research Center Cleveland,Ohio,NASA/TP-2002-211556,2002 被引量:1
  • 7Jiang Zonglin,Takayama Kazuyoshi,Chen Yaosong.Dispersion conditions for non-oscillatory shock capturing schemes and its applications.Computational Fluid Dynamics J,1995,4(2):137-150 被引量:1
  • 8Schultz E,Shepherd J.Validation of Detailed Reaction Mechanisms for Detonation Simulation,Graduate Aeronautical Laboratories,California Institute of Technology,Pasadena,Ca 91125,Explosion Dynamics Laboratory Report FM99-5,2000 被引量:1
  • 9Michael A.Nettleton,Gaseous Detonations:Their Nature,Effects and Control.New York:Chapman and Hall Ltd,1987.37-40 被引量:1
  • 10MA Fu-hua, Choi J, Yang V. Thrust chamber dynamics and propulsive performance of single-tube pulse detonation engines[J]. Journal of Propulsion and Power, 2005,21(3):512-526. 被引量:1

引证文献3

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部