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Analysis of the Flow around the Wing-in-Ground Effect Craft

Autor: Tetsuya, Kawamura

Publikováno v: 紀要 = BULLETIN OF SHIGA BUNKYO JUNIOR COLLEGE. 25:(85)-(96)

翼と地面の距離が小さくなると揚力が増加し、誘導抵抗が減少するという現象が起きる。この現象を地面効果とよび、地面効果を積極的に利用する乗り物を地面効果翼機（WIG）または表�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6ff371904ac26894b614cba86b02d630
http://id.nii.ac.jp/1656/00000116/

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Study of Circulation Control Wing aerodynamics design

Autor: Sasaki, Masafumi

Publikováno v: 宇宙航空研究開発機構特別資料: 第79回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 79th Meeting. :33-36

In this study, the aerodynamic performance of CCW (Circulation Control Wings) is investigated by two-dimensional (2D) CFD (Computational Fluid Dynamics) and the results are verified by 2D Wind-Tunnel-Test. It is found that CCW can achieve very higher

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::41d1849b66f172e25d91404fb94e8322
http://id.nii.ac.jp/1696/00005597/

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圧縮揚力による超音速デルタ翼の揚抗比増加に関する数値解析

Autor: Kanamori, Masashi, Imamura, Osamu, Suzuki, Kojiro

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. :17-21

We numerically analyze supersonic flows around a delta wing with bent wing tip. The results show that the lift and drag forces decrease with the increase in the bending angle. But the local augmentation is observed around the hinge line of bending in

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2aec49c7125e833af4b15e396c3cceaf
http://id.nii.ac.jp/1696/00005603/

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Research and development of PSP measurement system at JAXA 6.5 m x 5.5 m low-speed wind tunnel

Autor: Mitsuo, Kazunori, Kurita, Mitsuru, Kuchiishi, Shigeru, Fujii, Keisuke, Watanabe, Shigeya

Publikováno v: 宇宙航空研究開発機構特別資料: 第78回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 78th Meeting. :19-25

Pressure-Sensitive Paint (PSP) measurement system was developed in the JAXA 6.5 m x 5.5 m low-speed wind tunnel. Pressure images on a High-Lift-Device (HLD) model, which was built for R&D (Research and Development) for next generation of civil transp

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c88469868adf0c3958afdd558c59ebde
http://id.nii.ac.jp/1696/00005673/

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Present status of NAL's supersonic project (NEXST) and its perspectives

Autor: Sakata, Kimio

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). :423-427

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_______::ff74a4de932a80e470056581450fbcbc
http://id.nii.ac.jp/1696/00005777/

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Challenges of aircraft design integration

Autor: Kafyeke, F., Abdo, M., Pepin, F., Piperni, P., Laurendeau, E.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6fb2a14bbdb0d0284b906210637b1bf8
http://id.nii.ac.jp/1696/00005778/

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Aerodynamic design of the scaled supersonic experimental airplane

Autor: Shinbo, Yuichi, Yoshida, Kenji, Iwamiya, Toshiyuki, Takaki, Ryoji, Matsushima, Kisa

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_______::5274be51f30a076aac14bc63cf4ad9a7
http://id.nii.ac.jp/1696/00005735/

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Optimized design

Autor: Jeong, Shinkyu, Makino, Yoshikazu, Suzuki, Kenichiro, Ueda, Yoshine, Matsushima, Kisa, Yoshida, Kenji

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1cc7ef63550d81da8544f158bdea5f6b
http://id.nii.ac.jp/1696/00005780/

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CFD analysis applied to the supersonic research airplane

Autor: Takaki, Ryoji, Iwamiya, Toshiyuki, Aoki, Akiko

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::89ba76614b63a44e374d5bae4852305b
http://id.nii.ac.jp/1696/00005736/

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Numerical simulation with bleed and bypass effects of nacelles on SST

Autor: Kaiden, Takeshi, Shibata, Makoto, Iwamiya, Toshiyuki

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::662874516feff075d7bc2cf407e8d21e
http://id.nii.ac.jp/1696/00005727/

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