REVIEW - THE USE OF KIRCHHOFFS METHOD IN COMPUTATIONAL AEROACOUSTICS

被引：113
作者：
LYRINTZIS, AS [1 ]
机构：
[1] UNIV MINNESOTA, MINNEAPOLIS, MN 55455 USA
来源：
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME | 1994年 / 116卷 / 04期
关键词：
D O I：
10.1115/1.2911834
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
A comprehensive review of the use of Kirchhoff's method in computational aeroacoustics is given. Kirchhoff's integral formulation allows radiating sound to be evaluated based on quantities on an arbitrary control surface S if the wave equation is assumed outside. The control surface S is assumed to include all the nonlinear flow effects and noise sources. Thus only surface integrals are needed for the calculation of the far-field sound. A numerical CFD method can be used for the evaluation of the flow-field solution in the near-field and thus on surface S. Kirchhoff's integral formulation has been extended to an arbitrary, moving deformable piecewise-continuous surface. The available Kirchhoff formulations are reviewed and various aeroacoustic applications are given. The relative merits of Kirchhoff's method are also discussed.
引用
收藏
页码：665 / 676
页数：12
相关论文
共 98 条
  • [41] MECHANISMS AND DIRECTIVITY OF UNSTEADY TRANSONIC FLOW NOISE
    LYRINTZIS, AS
    LEE, J
    XUE, Y
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1994, 116 (03): : 649 - 652
  • [42] USE OF THE KIRCHHOFF METHOD IN ACOUSTICS
    LYRINTZIS, AS
    GEORGE, AR
    [J]. AIAA JOURNAL, 1989, 27 (10) : 1451 - 1453
  • [43] LYRINTZIS AS, 1994, 32ND AIAA AER SCI M
  • [44] LYRINTZIS AS, 1988, THESIS CORNELL U ITH
  • [45] LYRINTZIS AS, 1989, AM HELICOPTER SOC J, V34, P30
  • [46] LYRINTZIS AS, 1994, 115TH ASME C CHIC
  • [47] LYRINTZIS AS, 1992, INT S FLOW INDUCED V, V3, P85
  • [48] LYRINTZIS AS, 1995, 33RD AER SCI M REN
  • [49] LYRINTZIS AS, 1994, 50TH P AHS ANN FOR A, V1, P115
  • [50] LYRINTZIS AS, 1993, COMPUTATIONAL AERO H, V147, P53
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