Surface reflection: On the convergence of a series solution to a modified Helmholtz integral equation and the validity of the Kirchhoff approximation

1986 ◽  
Vol 79 (1) ◽  
pp. 64-70 ◽  
Author(s):  
Diana F. McCammon ◽  
Suzanne T. McDaniel
1999 ◽  
Vol 121 (2) ◽  
pp. 214-220
Author(s):  
Shu-Wei Wu

In the proposed approach, an acoustic domain is split into two parts by an arbitrary artificial boundary. The surrounding medium around the vibrating surface is discretized with finite elements up to the artificial boundary. The constraint equation specified on the artificial boundary is formulated with the Helmholtz integral equation straightforwardly, in which the source surface coincides with the vibrating surface discretized with boundary elements. To ensure the uniqueness of the numerical solution, the composite Helmholtz integral equation proposed by Burton and Miller was adopted. Due to the avoidance of singularity problems inherent in the boundary element formulation, this method is very efficient and easy to implement in an isoparametric element environment. It should be noted that the present method also can be applied to thin-body problems by using quarter-point elements.


Author(s):  
Grygorij S. Tymchik ◽  
Maryna V. Filippova ◽  
Oleg S. Bezverkhyi ◽  
Waldemar Wójcik ◽  
Bakhyt Yeraliyeva ◽  
...  

2016 ◽  
Vol 24 (01) ◽  
pp. 1550016 ◽  
Author(s):  
Steffen Marburg

The phenomenon of irregular frequencies or spurious modes when solving the Kirchhoff–Helmholtz integral equation has been extensively studied over the last six or seven decades. A class of common methods to overcome this phenomenon uses the linear combination of the Kirchhoff–Helmholtz integral equation and its normal derivative. When solving the Neumann problem, this method is usually referred to as the Burton and Miller method. This method uses a coupling parameter which, theoretically, should be complex with nonvanishing imaginary part. In practice, it is usually chosen proportional or even equal to [Formula: see text]. A literature review of papers about the Burton and Miller method and its implementations revealed that, in some cases, it is better to use [Formula: see text] as coupling parameter. The better choice depends on the specific formulation, in particular, on the harmonic time dependence and on the fundamental solution or Green’s function, respectively. Surprisingly, an unexpectedly large number of studies is based on the wrong choice of the sign in the coupling parameter. Herein, it is described which sign of the coupling parameter should be used for different configurations. Furthermore, it will be shown that the wrong sign does not just make the solution process inefficient but can lead to completely wrong results in some cases.


2014 ◽  
Vol 8 ◽  
pp. 2181-2194
Author(s):  
Nejmaddin A. Sulaiman ◽  
Shahraddin bin Sallah ◽  
Talhat I. Hassan

1971 ◽  
Vol 22 (1) ◽  
pp. 83-100 ◽  
Author(s):  
J. M. R. Graham

SummaryA method of obtaining the load distribution on thin rectangular wings in non-stationary incompressible flow is presented, with particular reference to the problem of gust-induced loading. The method utilises solutions to a Fourier transform of the downwash integral equation, enabling the problem to be expressed in the form of a set of dual integral equations having a series solution. Some values of the overall lift coefficient are computed and compared with values of lift coefficient obtained by collocation methods. The method is easily extendable to subsonic compressible flows.


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