Sensitivity Analysis of Unsteady Flow Fields and Numerical Experiments for Optimal Measurement
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説明
5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan
Difficulty of data assimilation arises from a large difference between the sizes of a state vector to be determined, i.e., the number of spatiotemporal grid points of a discretized numerical model, and a measurement vector, i.e., amount of measurement data. Flow variables on a large number of grid points are hardly defined by spatiotemporally limited amount of measurement data that poses an underdetermined problem. In this study we conduct sensitivity analysis of a vortex flow field by the use of an adjoint method. The idea of optimal/targeted observation in meteorology which aim to effectively determine a flow state by limited observations is interpreted in fluid dynamic problems where unsteady flows of much smaller scales are of interest.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA0062070015
レポート番号: JAXA-SP-13-001E
収録刊行物
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- 宇宙航空研究開発機構特別資料 = JAXA Special Publication
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宇宙航空研究開発機構特別資料 = JAXA Special Publication JAXA-SP-13-001E 209-215, 2013-11-30
宇宙航空研究開発機構(JAXA)
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詳細情報 詳細情報について
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- CRID
- 1050292561218829952
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- NII論文ID
- 120006827897
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- NII書誌ID
- AA11984031
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- ISSN
- 1349113X
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- Web Site
- http://id.nii.ac.jp/1696/00004117/
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- 本文言語コード
- en
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- 資料種別
- conference paper
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- データソース種別
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- IRDB
- CiNii Articles