PAME tools for RCS prediction and NCTI applications: Methodology and prediction for the French channel model

J. Simon, A. Cheraly
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Abstract

This paper is based on research conducted by ONERA the French Aerospace Lab) for efficiently calculate the RCS of an air intake of an aircraft. The multidomain and multi-method (MD2M) coupling scheme, called FACTOPO [1], is based on generalized scattering matrix computation on three-dimensional subdomains. The global target is split in NV subdomains (Vi) separed by NI fictitious surfaces Γj (Figure 1. ). We use a modal representation of the tangent fields on the interfaces. In each domain, the generalized Scattering matrix Si is computed independently of the others using the most appropriate method (MLFMM, direct solver taking into account symmetries [2], asymptotic method …). This coupling scheme leads to an important reduction in computational resources. The advantages of this formulation for parametric studies will be illustrated by the computing of the RCS of an air-intake with turning engine.
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用于RCS预测和NCTI应用的PAME工具:法国信道模型的方法和预测
本文是基于ONERA(法国航空航天实验室)为有效计算飞机进气道RCS而进行的研究。多域多方法(MD2M)耦合方案FACTOPO[1]是基于三维子域上的广义散射矩阵计算。全局目标被分成NV子域(Vi),这些子域由NI虚拟表面Γj分隔(图1)。. 我们使用接口上切线场的模态表示。在每个域中,使用最合适的方法(MLFMM、考虑对称性的直接求解器[2]、渐近方法等)独立计算广义散射矩阵Si。这种耦合方案大大减少了计算资源。该公式在参数化研究中的优点将通过计算一个旋转发动机进气的RCS来说明。
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