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Rarefied aerodynamic measurements in hypersonic rarefied wind tunnel
https://jaxa.repo.nii.ac.jp/records/39549
https://jaxa.repo.nii.ac.jp/records/39549a9a2073c-aca7-4172-8c9a-a37562776707
| Item type | 会議発表論文 / Conference Paper(1) | |||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-09-04 | |||||||||||
| タイトル | ||||||||||||
| タイトル | Rarefied aerodynamic measurements in hypersonic rarefied wind tunnel | |||||||||||
| 言語 | en | |||||||||||
| 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_5794 | |||||||||||
| 資源タイプ | conference paper | |||||||||||
| アクセス権 | ||||||||||||
| アクセス権 | metadata only access | |||||||||||
| アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||||||||
| 著者 |
Ozawa, Takashi
× Ozawa, Takashi
× Suzuki, Toshiyuki
× Fujita, Kazuhisa
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| 著者所属（英） | ||||||||||||
| en | ||||||||||||
| Japan Aerospace Exploration Agency(JAXA) | ||||||||||||
| 著者所属（英） | ||||||||||||
| en | ||||||||||||
| Japan Aerospace Exploration Agency(JAXA) | ||||||||||||
| 著者所属（英） | ||||||||||||
| en | ||||||||||||
| Japan Aerospace Exploration Agency(JAXA) | ||||||||||||
| 出版者（英） | ||||||||||||
| 出版者 | American Institute of Physics(AIP) | |||||||||||
| 書誌情報 |
en : AIP Conference Proceedings 巻 1628, 発行日 2014-12 |
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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 | 29th International Symposium on Rarefied Gas Dynamics(July 13-18, 2014.), Xi'an, China | |||||||||||
| 抄録（英） | ||||||||||||
| 内容記述タイプ | Other | |||||||||||
| 内容記述 | In order to improve the feasibility of space missions, the prediction accuracy of rarefied aerodynamics is one of the important factors. To improve rarefied aerodynamic predictions, the determination of accommodation coefficients and direct measurement of rarefied aerodynamic forces are crucial. Thus, at Japan Aerospace Exploration Agency, a hypersonic rarefied wind tunnel has been developed for rarefied aerodynamic measurements. In this work, we have utilized both experimental and numerical approaches for rarefied hypersonic aerodynamic measurements, and the measurement schemes have been developed by using pendulous models for accommodation coefficients and for aeroshell aerodynamic characteristics. Consequently, we have successfully demonstrated measurements of accommodation coefficients and rarefied aerodynamic characteristics for an aeroshell. | |||||||||||
| ISBN | ||||||||||||
| 識別子タイプ | ISBN | |||||||||||
| 関連識別子 | 978-0-7354-1265-1 | |||||||||||
| DOI | ||||||||||||
| 識別子タイプ | DOI | |||||||||||
| 関連識別子 | http://dx.doi.org/10.1063/1.4902739 | |||||||||||
| 関連名称 | info:doi/10.1063/1.4902739 | |||||||||||
| 資料番号 | ||||||||||||
| 内容記述タイプ | Other | |||||||||||
| 内容記述 | 資料番号: PA1510081000 | |||||||||||
