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Aerodynamic design of supersonic experimental airplane

Autor: Iwamiya, Toshiyuki, Yoshida, Kenji, Shinbo, Yuichi, Makino, Yoshikazu, Matsushima, Kisa

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). :274-279

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
超音速輸送機に対するNALの実験(NEXST(小型超音速実験機計画)-1)の第1段階において、超音速航�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::66df18c4d3ae9dcbc771a42dec6fecdc
http://id.nii.ac.jp/1696/00005755/

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Comparison of structured and unstructured grids on generic helicopter fuselage with a rotor

Autor: Yang, Choongmo, Nam, Hwajin, Kwon, Ohjoon, Aoyama, Takashi, Saito, Shigeru

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. :29-34

Helicopters are used in various fields such as EMS (Emergency Medical Service), fire fighting, disaster relief, news report, and so on because of the capabilities of hovering and VTOL. However, noise, cost, and VFR (Vision Flight Rules) problems prev

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9ad5b300475b7afd4c4a91f19dc4727c
http://id.nii.ac.jp/1696/00006131/

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Experimental analysis of the effect of side walls of a linear aerospike nozzle on the jet-flow structure

Autor: Mori, Hideo, Taniguchi, Mashio, Nishihira, Ryutaro, Niimi, Tomohide

Publikováno v: 宇宙航行の力学シンポジウム平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004. :120-123

資料番号: AA0048089031

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b017d855c26a05231e94c67816638e49
http://id.nii.ac.jp/1696/00014632/

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Effects of the fuselage shape on aerodynamic characteristics of reusable spacecraft

Autor: Morita, Wataru, Aso, Shigeru, Tani, Yasuhiro, Tadakuma, Kenji, Tsuchiya, Shigeki, Nishimura, Mitsumasa, Irikado, Tomoko, Sato, Kiyoshi

Publikováno v: 宇宙航行の力学シンポジウム平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004. :110-113

資料番号: AA0048089028

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::32b3746502600cfa729f50f308e01880
http://id.nii.ac.jp/1696/00014629/

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再使用推進系の総合研究:(1)信頼性設計手法の検討(2)再使用推進系総合計画

Autor: Kuratani, Naoshi, Taguchi, Hideyuki, Himeno, Takehiro, Hasegawa, Takuya, Aoki, Hiroshi

Publikováno v: 宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System. :9-14

Synthetic studies on the reusable and future propulsion systems are presented in this paper. Especially, focused are the high reliability design methodology for the liquid rocket engine at conceptual phase, the flight demonstration project SubLEO tha

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4c9cc4e6d5ff06d1ca57c58564765a27
http://id.nii.ac.jp/1696/00002728/

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Calculation of rotor/fuselage interaction using overlapped grid method

Autor: Kondo, Natsuki, Aoyama, Takashi, Saito, Shigeru

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2003論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003. :232-237

This paper presents rotor aerodynamic analysis including influence of a fuselage using an unsteady Euler code. A moving overlapped grid method is applied in the code and four types of grid, inner and outer background grids, blade grid, and fuselage g

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::209125e320bfdb1cd59c873e0545040c
http://id.nii.ac.jp/1696/00006636/

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CFD application to helicopter configuration

Autor: Uchiyama, Naoki

Publikováno v: 航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2002論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002. 57:298-303

The in-house rotor CFD code has been further developed to apply for aerodynamic issues on realistic helicopter configuration. The code solves the unsteady Euler equations for flowfield around helicopter in forward flight with rotor blades in cyclic m

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::37d152a60af854582d7841d8710e1479
http://id.nii.ac.jp/1696/00038268/

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