4次元変分法による後方乱気流の計測融合シミュレーション  [in Japanese] Measurement-Integrated Simulation of Wake Turbulence with Four-Dimensional Variational Method  [in Japanese]

Abstract

空港における実運航機の後方乱気流の解析は大気境界層や飛行経路を考慮する必要から一般に困難である.本研究では仙台空港において離陸機の後流をライダ計測し,その計測値を数値流体力学シミュレーションに融合する手法を開発した.ライダ計測値は4次元変分法により実際の計測プロセスを模擬しながら同化した.本論文では手法を説明した後,ライダ計測値の同化過程と再現された後方乱気流の挙動に関して議論する.

Realistic retrieval of aircraft wake turbulence at an airport is not straight-forward due to the difficulty in incorporating actual conditions such as an atmospheric boundary layer and a flight trajectory into the numerical simulation. In this study, the numerical simulation of wake turbulence is performed by integrating lidar measurements at Sendai airport. The four-dimensional variational method is employed for the integration with taking an actual measurement process into consideration. The behavior of wake turbulence under realistic wind conditions is shown after the discussion regarding the convergence of a retrieved flow field.

Journal

Bulletin of the Japan Society for Industrial and applied Mathematics   [List of Volumes]

Bulletin of the Japan Society for Industrial and applied Mathematics 19(3), 150-162, 2009-09-25  [Table of Contents]

The Japan Society for Industrial and Applied Mathematics

References:  19

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Codes

  • NII Article ID (NAID) :
    110007361023
  • NII NACSIS-CAT ID (NCID) :
    AN10288886
  • Text Lang :
    JPN
  • Article Type :
    ART
  • ISSN :
    09172270
  • NDL Article ID :
    10455340
  • NDL Source Classification :
    ZM31(科学技術--数学)
  • NDL Call No. :
    Z15-726
  • Databases :
    CJP  NDL  NII-ELS 

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