非構造移動重合格子解析プログラム (FaSTAR-Move) の回転翼解析への拡張

書誌事項

タイトル別名
  • Development of Unstructured Overset Grid CFD Solver FaSTAR-Move for Flow Analysis Around Rotorcraft

抄録

第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム (2019年7月1日-3日. 早稲田大学早稲田キャンパス国際会議場), 新宿区, 東京

51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium (July 1-3, 2019. International Conference Center, Waseda University), Shinjuku-ku, Tokyo, Japan

A CFD solver “FaSTAR-Move” that enables analysis around moving and deformed objects have been developed by JAXA, and was applied to the analysis of separation of mounted objects, etc. Currently, the rotorcraft analysis module has been added to FaSTAR-Move in order to meet industrial needsdemands for the rotorcraft analysis . In this paper, comparisons and validations of the developed module with experiments of hovering rotor are performed and it is shown that reasonable results are obtained.

形態: カラー図版あり

Physical characteristics: Original contains color illustrations

資料番号: AA1930011017

レポート番号: JAXA-SP-19-007

収録刊行物

詳細情報 詳細情報について

  • CRID
    1050011086284898048
  • NII論文ID
    120006839158
  • ISSN
    24332232
  • Web Site
    http://id.nii.ac.jp/1696/00046347/
  • 本文言語コード
    ja
  • 資料種別
    conference paper
  • データソース種別
    • IRDB
    • CiNii Articles

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