Výsledky vyhledávání - "よどみ点圧力"

Flow characteristics of UT-Kashiwa hypersonic wind tunnel

Autor: Imamura, Osamu, Watanuki, Tadaharu, Suzuki, Kojiro, Kashiwa Wind Tunnel Working Group

Publikováno v: 宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :50-55

In this study, the flow characteristics of UT (University of Tokyo)-Kashiwa hypersonic wind tunnel are obtained by measuring the Pitot pressure distribution. In this wind tunnel, the Mach 7 and 9 hypersonic nozzles are inherited from its predecessor

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fe716620dfdd9bdc17c0740b21e8b804
http://id.nii.ac.jp/1696/00005609/

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Preliminary report of the blockage data in JAXA 1 m x 1 m Supersonic Wind Tunnel

Autor: Iijima, Hidetoshi, Sato, Mamoru, Watanabe, Mitsunori, Nagai, Shinji, Itabashi, Yukihiro, Nishijima, Hironori, Kimura, Takeshi

Publikováno v: 宇宙航空研究開発機構特別資料: 第76回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 76th Meeting. :33-37

JAXA1m×1m超音速風洞における風洞始動限界を、異なるブロッケージ比の円盤および正方形板模型を用いて調べた。また、その妥当性を確認するために、他風洞の結果と比較した。さらに、

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::51b31fae18f78507da815fa074476066
http://id.nii.ac.jp/1696/00005836/

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JAXA極超音速風洞で用いている気体モデル

Autor: Watari, Minoru

Publikováno v: 宇宙航空研究開発機構特別資料: 第76回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 76th Meeting. :23-26

Three air models are used in JAXA hypersonic wind tunnel. They are 'perfect', 'thermally perfect', and 'real' models. Thermally perfect model considers an atomic-vibration energy. Real model considers an atomic vibration and an inter-molecular potent

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e38ace8dfbcff396d5c02fddc01339f0
http://id.nii.ac.jp/1696/00005833/

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Diagnosis of air condensation in hypersonic flow

Autor: Yamazaki, Takashi, Nakakita, Kazuyuki, Inoue, Yasutoshi, Soga, Kunio

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 38:219-228

22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)
NAL中型衝撃風洞とRCS(リアクションコントロールサブシステム)試験用ガス混合装置を用いて極超音速流のAir Condensationをピトー圧力波形によって診断�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::35ccf23372d6ca7fec419fdd454ac088
http://id.nii.ac.jp/1696/00037195/

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Flow-deflection characteristics of JAXA 0.44 m Hypersonic Shock Tunnel with a dual-wheel model support system

Autor: Yamazaki, Takashi, Nakakita, Kazuyuki, Nakagawa, Muneyoshi, Watari, Minoru