RCS Computation of 3D-wake Vortex Using Method of Moments
An efficient and accurate 3D full wave numerical solution model for computing the radar cross section (RCS) of wake-vortex is presented, by solving Euler equation to compute the pressure in the aircraft wake region by computational fluid dynamics model and parallel integral equation (IE), based on method of moments (MoM) is used to compute the volume polarization currents, under the plane wave incidence. Then the currents are used to compute far-field from the vortex region.
Venkat Prasad Padhy N.Balakrishnan P.Srinivasa Murthy
SERC, Indian Institute of Science, Bangalore 560012, India Aeronautical Development Establishment (ADE), Bangalore 60075, India
国际会议
Progress in Electromagnetics Research Symposium 2014(2014年电磁学研究新进展学术研讨会)
广州
英文
1319-1322
2014-08-01（万方平台首次上网日期，不代表论文的发表时间）