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Measurements of the Aerodynamic Derivatives of an Oscillating Biconvex-Flat Airfoil in Supersonic Flow at Mach Number 2 to 3
https://jaxa.repo.nii.ac.jp/records/44296
https://jaxa.repo.nii.ac.jp/records/44296eefa9e81-b27b-4a15-9971-fc8c39b11580
名前 / ファイル | ライセンス | アクション |
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naltr0057t.pdf (3.4 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 | Measurements of the Aerodynamic Derivatives of an Oscillating Biconvex-Flat Airfoil in Supersonic Flow at Mach Number 2 to 3 | |||||
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 | |||||
著者 |
ISHII, Takao
× ISHII, Takao× YANAGIZAWA, Mitsunori |
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著者所属(英) | ||||||
en | ||||||
National Aeronautical Laboratory First Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
Nippon Oil Seal Industry Co., Ltd., First Aerodynamics Division, National Aeronautical Laboratory(NAL) | ||||||
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 |
en : Technical Report of National Aerospace Laboratory TR-57T 巻 57T, p. 17, 発行日 1964-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The aerodynamic derivatives of a biconvex-flat airfoil (thickness ratio of 10 per cent), and double-wedge airfoils (thickness ratios of 10, 15, 20 percent), performing pitching oscillation in supersonic flow at the range of Mach number2-3, were measured and compared with the linearized theory, piston theory and Van Dyke's nonlinear theory which includes the effect of the airfoil thickness. The tested reduced frequency range was 0.01-0.05 and the Reynolds number range was 2.8 by 10(6)-3.6 by10(6) based on the chord length. In spite of the existence of the detached shock wave in front of the leading edge of the biconvex-flat airfoil, all experimental results agree quite well with the nonlinear theory. Schlieren photographs were taken in order to observe the flow field around the airfoils. | |||||
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: NALTR0057T000 | |||||
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-57T |