WEKO3
アイテム
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A comparative study of BGK No.1 airfoil data in high Reynolds number transonic wind tunnels
https://jaxa.repo.nii.ac.jp/records/41176
https://jaxa.repo.nii.ac.jp/records/411765615f5a3-c697-41a9-9a6f-848f4f0f8660
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr1191t.pdf (6.7 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A comparative study of BGK No.1 airfoil data in high Reynolds number transonic wind tunnels | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 対応風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞データ比較 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速高レイノルズ数風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ2次元性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞側壁境界層効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞壁干渉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞性能評価 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型データ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | BGK翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | バウアー・ガラベディアン・コーン翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速空気力学 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel correlation test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel data comparison | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic high Reynolds number wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel testing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow two dimensionality | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel sidewall boundary layer effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel wall interference | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel performance assessment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil data | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | BGK airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Bauer Garabedian Korn airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic aerodynamics | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | 高レイノルズ数遷音速風洞におけるBGK No.1翼型データの比較研究 | |||||
著者 |
須谷, 記和
× 須谷, 記和× 松野, 謙一× 神田, 宏× 佐藤, 衛× 三輪, 等× 河本, 巌× Sudani, Norikazu× Matsuno, Ken-ichi× Kanda, Hiroshi× Sato, Mamoru× Miwa, Hitoshi× Kawamoto, Iwao |
|||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory 巻 1191T, p. 1-137, 発行日 1993-01 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | BGK No.1翼型に関する対応風洞試験が航空宇宙技術研究所(NAL)とカナダ国立航空研究所(IAR,旧NAE)の高レイノルズ数遷音速翼型試験設備において実施された。試験はレイノルズ数(翼弦長基準)21×10{6}を中心として低亜音速域から設計点を越える速度域まで実施され、圧力分布や空力係数の比較検討を行った。その結果、衝撃波の位置や衝撃波上流での圧力係数値に微妙な相違が認められ、側壁干渉効果補正の必要性が示唆された。そこで、ある側壁干渉補正法を適用したところ両者の測定結果は良好な一致を示すことが確認された。また、この試験により大仰角あるいは高マッハ数での抵抗測定の精度向上や流れの2次元性の確保などの新たな問題点が浮き彫りにされ、高精度の翼型試験の実現のための有益な資料を得ることができた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A comparative study of BGK (Bauer Garabedian Korn) No. one airfoil data in the NAL (Japan) and IAR (Institute for Aerospace Research, Canada) high Reynolds number transonic wind tunnels was performed to evaluate the techniques and the accuracy of airfoil testing. Tests were conducted from a low subsonic speed over the design speed of the airfoil mainly at a Reynolds number of 21 million based on airfoil chord at both facilities. Pressure distributions and aerodynamic characteristics measured in both wind tunnels are compared and discussed. The results of the comparisons reveal slight differences in shock position and suction peak level ahead of the shock, suggesting the necessity of a correction for sidewall boundary-layer effects. Application of sidewall interference correction to both sets of wind tunnel data improves agreement between the two sets of data. The results also raise new issues on drag measurement and flow two dimensionality at a high angle of attack and/or a high Mach number. The results of this study will lead to improvements in the accuracy of airfoil testing. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0004206000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1191T |