采用波浪绕射理论和源汇法对悬浮隧道所受波浪荷载进行了求解。
On the basis of diffraction theory the wave loading on an SFT was solved by the source distribution method;
本文提供了用超音速源汇法计算任意三维机翼超音速厚度压强分布的算法语言程序。
This paper presents a ALGOL program for calculating the thickness pressure distributions of arbitrary supersonic three dimensional wings by using the method of source singularities.
经典圆定理只证明了奇点位于圆外的情况，本文用正则摄动法证明了源和汇位于圆上时，圆定理也是适用的。
This study illustrated that the theorem could be also applied in a case where the sources and sinks are on the circle by means of the regular perturbation method.
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