Study on Mesh Generation Method for Fluid Analysis Around Supersonic Aircraft

DOI Web Site

Bibliographic Information

Other Title
  • 超音速飛翔体周りの流体解析に対する格子生成法の研究

Abstract

<p>In this study, numerical analysis for predicting near-field pressure signatures of supersonic airplane validated to use Automatic Hexahedra Grid Generation Method "HexaGrid" and Fast Unstructured CFD Code "FaSTAR". The model configuration first phase of JAXA's low-sonic-boom concept demonstration project(D-SEND#1) is used in this study. As a result, it was found that high density of grid and shock waves need to be aligned with Cartesian gird in order to accurately grasp near-field pressure signatures of supersonic airplane.</p>

Journal

Keywords

Details 詳細情報について

Report a problem

Back to top