Construction of the linear reduced-order model based on PIV data of flow field around airfoil

研究成果: Conference contribution

抄録

In this study, a linear reduced-order model of flow fields around the NACA0015 for an observer of active flow control system is constructed based on the time-resolved particle image velocimetry (PIV) data, and its behavior and accuracy are investigated. The PIV data were obtained at the chord Reynolds number of 6.0 × 104, and the angle of attack of from 11° to 20°. Proper orthogonal decomposition (POD) analysis is employed to the PIV data and degrees of freedom of data are reduced by truncating the POD modes. Then, the linear model of POD modes is constructed by the least squares method based on the obtained time history of POD modes. Although the estimated time advancement of POD modes by the model reproduces the time history of the original data at the beginning, it gradually attenuates and finally converges to zero. This behavior is also supported by the eigenvalue analysis results of coefficient matrices of the linear model. In addition, behavior of the low-order (more energetic) POD modes was reproduced better than high-order (less energetic) POD modes. The results imply that temporal fluctuation of large vortex structures has strong linearity, and is not significantly affected by noise included in data. The former insight is also supported by the fact that the POD modes were reproduced well in the case of high angle of attack.

本文言語English
ホスト出版物のタイトルAIAA Scitech 2019 Forum
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105784
DOI
出版ステータスPublished - 2019 1 1
イベントAIAA Scitech Forum, 2019 - San Diego, United States
継続期間: 2019 1 72019 1 11

出版物シリーズ

名前AIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
国/地域United States
CitySan Diego
Period19/1/719/1/11

ASJC Scopus subject areas

  • 航空宇宙工学

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