Výsledky vyhledávání - "超音速飛行"

Study of flow structures around vehicle traveling at supersonic/hypersonic speeds

Autor: Nakamura, Hiroaki, Manabe, Keiji, Sezaki, Shinji, Nishio, Masatomi

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :47-50

Flow structures around a hypersonic re-entry Mars Environmental Survey (MESUR) capsule traveling at supersonic/hypersonic speeds are investigated utilizing a new computational method based on the finite element method (FEM). In order to confirm the v

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0857235215efc7e6b9c32d816941cceb
http://id.nii.ac.jp/1696/00014652/

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気球から自由落下する飛翔体における超音速飛行と引き起こし制御の検討

Autor: Kadooka, Shohei, Sawai, Shujiro, Bando, Nobutaka, Sakai, Shinichiro, Watanabe, Rikio, Hashimoto, Tatsuaki

Publikováno v: 第17回アストロダイナミクスシンポジウム講演後刷り集 2007 = Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics. :333-337

現在ISAS/JAXAでは気球を用いた微小重力実験装置の開発を進めている。この実験は、(1)高高度気球で高度40kmまで上昇させる、(2)実験機体を切り離す、(3)30-40秒間の自由落下を実現するもの�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2c175bfef643fda31c45467ec61fc318
http://id.nii.ac.jp/1696/00007486/

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Inverse design of biplane airfoils for efficient supersonic flight: Preliminary trial to construct biplane airfoil data base

Autor: Maruyama, Daigo, Matsushima, Kisa, Kusunose, Kazuhiro, Nakahashi, Kazuhiro

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling. :195-205

There is a biplane concept for an efficient supersonic flight. Busemann biplane is a representative airfoil which has possibility of realizing low-boom and low wave drag. Aerodynamic designs based on the Busemann biplane are demanded for future super

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::817d5919fdefbcae13c8a003eab2fcb1
http://id.nii.ac.jp/1696/00005669/

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Experimental study on the unsteady effects in supersonic flight

Autor: Khalil, Mohammed, Saso, Akihiro, Nakamura, Yoshiaki, Sakai, Takeharu, Mori, Koichi

Publikováno v: 宇宙航空研究開発機構契約報告: サイレント超音速機に関する調査研究:平成18年(2006年)度研究成果報告書 = JAXA Contract Report: Survey and Research on Silent Supersonic Aircraft: Report on the Research Results of FY2006. :86-101

資料番号: AA0063603005
レポート番号: JAXA-CR-07-001

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b050ae52e73cad1c5e25ec21db485d66
http://id.nii.ac.jp/1696/00006677/

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Optimization of nose shape for reduction of sonic boom

Autor: Yamaguchi, Hayato, Nakamura, Yoshiaki

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop). :128-131

SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design 航空宇宙技術研究所 19980316-19980317 東京日本
SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laborato

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6014336ba48c5b8e1ec1241a493d17d7
http://id.nii.ac.jp/1696/00005742/

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CFD activity for future winged space transport system

Autor: Yamamoto, Yukimitsu, Kurotaki, Takuji

航空宇宙技術研究所 17-19 Jan. 2000 東京日本
National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan
NAL(航空宇宙技術研究所)においては、NASDA(宇宙開発事業団)との共同研究として、大気圏宇宙�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::c059a8c02a5f8817e8f88bbd73a998f0
http://id.nii.ac.jp/1696/00005769/

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Low sonic-boom design using numerical optimization

Autor: Makino, Yoshikazu, Kubota, Hirotoshi, Aoyama, Takashi, Iwamiya, Toshiyuki

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a2dacab5f206b664569717ee7b510c96
http://id.nii.ac.jp/1696/00005741/

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再突入宇宙機の横方向制御:エルロン逆効きロールとヨーRCSロール

Autor: Yonemoto, Koichi

Publikováno v: 第15回アストロダイナミクスシンポジウム講演後刷り集 2005 = Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics. :401-406

再突入飛行時に非常に大きな迎角で飛行する有翼式再突入機は、横方向の安定性と制御性に関する困難な問題に直面する。本論文は、我が国の宇宙往還技術試験機HOPE-X(H-2 Orbiting Plane-Expri

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e0ff32d49b9155db42a14e5f28cc0669
http://id.nii.ac.jp/1696/00007621/

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Proposal of FTB system, an air breathing engine

Autor: Tokudome, Shinichiro, Habu, Hiroto, Kawaguchi, Junichiro, Otsuka, Hirohito, Yamamoto, Takayuki

Publikováno v: 第5回宇宙科学シンポジウム = Proceedings of the 5th Space Science Symposium. :400-403

本稿では、完全再使用宇宙輸送系の構築へ向けた最初の1歩として、ロケット複合サイクル推進系の開発が急務であり、それを早期に実現するためには、飛翔実験装置(FTB=Flying Test Bed)の開

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http://id.nii.ac.jp/1696/00011346/

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Study on flowfield around winged TSTO launch vehicle by visualization using the electrical discharge method

Autor: Sezaki, Shinji, Nakamura, Hiroaki, Nishio, Masatomi, Yamamoto, Yukimitsu

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :119-122

The visualization of flowfield around a winged TSTO (Two Stage To Orbit) launch vehicle model has been carried out using the electrical discharge method. In this report, boundary layers and three-dimensional (lateral and cross-sectional) shock shapes

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::384ccbecba9229c50e5d05c0dfe931d8
http://id.nii.ac.jp/1696/00014670/

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