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Wall Interference Analysis by Whole Wind Tunnel CFD
https://jaxa.repo.nii.ac.jp/records/4116
https://jaxa.repo.nii.ac.jp/records/4116f2bedea9-ca6f-4347-ae7c-55982155766c
名前 / ファイル | ライセンス | アクション |
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62070008.pdf (522.1 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Wall Interference Analysis by Whole Wind Tunnel CFD | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Wall interference | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
著者 |
橋本, 敦
× 橋本, 敦× 香西, 政孝× Hashimoto, Atsushi× Kohzai, Masataka |
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著者所属 | ||||||
宇宙航空研究開発機構研究開発本部数値解析グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部数値解析グループ(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication 巻 JAXA-SP-13-001E, p. 103-113, 発行日 2013-11-30 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | For wall interference correction, the potential-based methods such as Mokry’s method are commonly used. In fact, the linear correction methods cannot be used for transonic and stall conditions. In this study, the Mokry’s method is applied to wind tunnel CFD, and the corrected aerodynamic coefficients are compared with CFD without wall to investigate validity and limitation of the method. We have simulated the whole wind tunnel flow of JAXA 2m×2m Transonic Wind Tunnel (JTWT). The pressure distribution on the wind tunnel wall agrees well with the measurements. In addition, the computed C(L) and C(D) agree well with the measured values. The differences between standard and long stings are almost same as the experiment. It is found that the aerodynamic characteristics of ONERA-M5 and its wall/support interferences are well reproduced in this computation. In the case of M=0.7, long sting, and α=0 deg, the results corrected by the Mokry’s method show good agreement with those without wall. However, the accuracy is degenerated by shock wave, separation, and support interference, since the Mokry’s method is based on the linear potential theory. It is found that the effect of support interference is not so large, whereas the effect of separation is serious. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062070008 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-13-001E |