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Investigation of ATP blades (Part II)-Validation of Two-dimensional Viscous Flow Simulation Codes around Thin Airfoils-
https://jaxa.repo.nii.ac.jp/records/45305
https://jaxa.repo.nii.ac.jp/records/453050e318c2e-43f7-4584-b6ca-602f7b91e62c
名前 / ファイル | ライセンス | アクション |
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naltr01046.pdf (2.3 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Investigation of ATP blades (Part II)-Validation of Two-dimensional Viscous Flow Simulation Codes around Thin Airfoils- | |||||
言語 | ||||||
言語 | eng | |||||
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 | ATPブレードの研究(II)-薄翼翼型廻り流れによる2次元粘性流解析コードの検証- | |||||
著者 |
福田, 正大
× 福田, 正大× 廣瀬, 直樹× 河合, 伸坦× 中橋, 和博× 菊野, 栄次× FUKUDA, Masahiro× HIROSE, Naoki× KAWAI, Nobuhiro× NAKAHASHI, Kazuhiro× KIKUNO, Eiji |
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著者所属 | ||||||
航空宇宙技術研究所数理解析部 | ||||||
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 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Computational Sciences Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Sumitomo Precision Products Co., Ltd. | ||||||
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 TR-1046 巻 1046, p. 24, 発行日 1989-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The two-dimensional Navier-Stokes codes, NSFOIL and NS2D, are validated in terms of analysis of practical thin-airfoils for conventional propeller systems and compared with data obtained from wind-tunnel tests. This research was done as part of an aerodynamic research project on propeller blades for advanced turboprop (ATP) engines. The comparison was made at a Reynolds number of 8 million which was equivalent to the actual flight condition of ATP, and it was shown that these codes provide very effective tools for predicting nonlinear characteristics of thin-airfoils. In the course of careful comparison, some improvements on these codes were clarified. | |||||
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: NALTR1046000 | |||||
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-1046 |