境界要素法による全機形状まわり超音速定常流の数値解析

概要

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A boundary element method program for steady supersonic flow is revised to enable to treat flow around wing-body configurations. The revision consists of three items ; 1) separation of panel-producing procedure and output procedure from the main calculation part in the program, 2) utilization of external storage to increase the ability to treat more complex configurations, 3) addition of wake calculation procedure which is necessary to deal with wind-body configurations correctly. Flow around AGARD-B standard model is calculated, and the result shows the consistency with a wind tunnel test, which ensures the validness of the present revision.
岡山理科大学の論文