Výsledky vyhledávání - "ソニックブーム"

An aerodynamic design method for generating low sonic-boom pressure signatures

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

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1406:1-19

コンコルドに代わる次世代SST(超音速輸送機)開発における環境適合性に関する課題の1つに、ソニックブームの低減化が挙げられる。ソニックブームを低減化させる方法としては、機体形�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::29399eea720ceeb233eb51934f69d597
http://id.nii.ac.jp/1696/00040623/

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Control of a flow field around a silent supersonic aircraft using a plasma actuator

Autor: Kawazoe, Hiromitsu, Matsuno, Takashi

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. :74-85

資料番号: AA0063603004
レポート番号: JAXA-CR-07-001

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b88f860a5fee7e537cab86cbb194d8ac
http://id.nii.ac.jp/1696/00006676/

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Study on the flight stability of biplane silent supersonic aircraft at takeoff and landing: Construction of a testbed for flight demonstration

Autor: Jeong, Shinkyu, Obayashi, Shigeru, Kawazoe, Hiromitsu, Matsuno, Takashi, Kuratani, Naoshi

資料番号: AA0063603002
レポート番号: JAXA-CR-07-001

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d688432599a989dac80186c053eb7aa7
http://id.nii.ac.jp/1696/00006674/

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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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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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Silent supersonic technology demonstrator project

Autor: Murakami, Akira

SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ: Toward the Future form NEXST-1 Flight Trial 宇宙航空研究開発機構 20061012-20061013 東京日本
SS

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::57cfb73fc68f409b5c29719c574e070d
http://id.nii.ac.jp/1696/00005796/

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Aerodynamical designing of the second generation supersonic transport (SST-2)

Autor: Vasiliev, L. E.

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
第2世代の超音速輸送機(SST-2)にはSST-1より高い効率性が要求されている。SST-2は亜音速および�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::2de717cddf5fc0fab39d1c77301fc8e3
http://id.nii.ac.jp/1696/00005749/

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Automated aerodynamic design optimization system for SST wing-body configuration

Autor: Yang, Guowei, Sasaki, Daisuke, Obayashi, Shigeru

SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ航空宇宙技術研究所 20011203-20011205 東京日本
SST-CFD Workshop. International Workshops on Numer

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::87045547989b6ea0520e6b1f7365435e
http://id.nii.ac.jp/1696/00005781/

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Low sonic-boom design of a silent supersonic technology demonstrator: Development of CAPAS and its application

Autor: Makino, Yoshikazu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0198e59f0aa445626ea5931fabfb8643
http://id.nii.ac.jp/1696/00005802/

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Aerodynamic design of low boom and low drag supersonic transport using favorable shock wave interference

Autor: Maruyama, Daigo, Nakano, Tomoharu, Matsushima, Kisa, Nakahashi, Kazuhiro

Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :132-137

In supersonic flight, airplanes cause strong sonic booms and wave drags resulted from shock waves. Kusunose has proposed a new concept for supersonic transport, whose sonic booms and wave drag can be significantly reduced, using a Busemann's Biplane

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bf46bb30c01aa94ec8a0a14b2f988a41
http://id.nii.ac.jp/1696/00006149/

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