Výsledky vyhledávání - "地面効果翼"

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-9. 9:223-228

Flow around an aircraft spatially designed to taking advantage of ground effect effectively is studied by using the incompressible Navier-Stokes equations. Third-order upwind difference scheme is used to solve the equations. Calculations are carried

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7f80f866e38355c8157646e261eecd4d
http://id.nii.ac.jp/1696/00043318/

Zobrazit plný text záznamu

地面効果翼機まわりの流れの数値シミュレーションII

Autor: Kawamura, Tetuya, Kubo, Shozo

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10. 10:243-248

Flow around a wing in ground effect is studied by solving both the incompressible and compressible Navier-Stokes equations numerically. Standard MAC method with third order upwind difference for non-linear term is used to calculate incompressible flo

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e3bbbbfeec108ae3892112fa80f43d50
http://id.nii.ac.jp/1696/00043364/

Zobrazit plný text záznamu

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/

Zobrazit plný text záznamu

地面効果内を飛行する3次元翼及び前翼式地面効果翼機の定常・非定常空力特性

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f8952f1ae9d5ea0c4c0f23ecd98f90b7
https://ir.lib.hiroshima-u.ac.jp/00043696

Zobrazit plný text záznamu

Experiments at the Sunrise-Beach Research Facility of the aerodynamic characteristics on ground effects of aerofoils with a secondary aerofoil

Autor: Takahashi, Yuji, Kikuchi, Masanori, Hirano, Kimitaka, Yuge, Toshio, Moriya, Taishi, Kohama, Yasuaki

Publikováno v: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集第40回 = JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition. :47-50

Investigation of a new high-speed zero-emission transportation 'Aerotrain' is proceeded mainly in Tohoku University and Miyazaki University. Since the aerotrain utilizes the ground effect, researches of the aerofoil section which can harnesses the gr

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::03fc82a1494956d5dcca91e1af4795fc
http://id.nii.ac.jp/1696/00005530/

Zobrazit plný text záznamu

Unsteady aerodynamic characteristics of wings in ground effect

Autor: Matsuzaki, Takahisa, Yoshioka, Shuya, Kato, Takuma, Kohama, Yasuaki

In spite of the great deal of effort has been made on researching the ground effect in the steady condition, little attention has been given to the ground effect in the unsteady condition. This paper is, therefore, intended as an investigation of the

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bd7b7f67e276cb3f976a270c91f30d4b
http://id.nii.ac.jp/1696/00005532/

Zobrazit plný text záznamu

Numerical simulation of flow-field around three dimensional WIG using multi-block code

Autor: Hirata, Nobuyuki

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 30:199-204

航空宇宙技術研究所 7-9 Jun. 1995 東京日本
National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan
地面効果翼(WIG)機は次世代超高速船の有望な候補の1つとして期待されている。WIGは地面に近づ�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c0d2b51fecaf9eea81cd02682a0db91e
http://id.nii.ac.jp/1696/00036797/

Zobrazit plný text záznamu

エアロトレインとその空力安定性

Autor: Kohama, Yasuaki P., Watanabe, Hideo, Kikuchi, Satoshi, Ota, Fukuo, Ito, Takatoshi

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. :77-80

航空宇宙技術研究所 27-29 Sept.2000 東京日本
National Aerospace Laboratory 27-29 Sept.2000 Tokyo Japan
地球の深刻な温室効果を考慮し、輸送システムからの2酸化炭素排出を防止する思い切った提

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3c8ad4e5673097bacbe0bf598dfc4a2d
http://id.nii.ac.jp/1696/00041407/

Zobrazit plný text záznamu

A numerical analysis of aerofoil flutter in ground effects

Autor: Kawahara, Takayuki, Kikuchi, Masanori, Hirano, Kimitaka

The 'Aero-train' flies in the close field above the ground using ground effects. It is important for Aero-train that making known the relationship between the Ground Effects and 'Flutter'. So we simulated Aerofoil Flutter in Ground Effects. We made w

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::072ed897d899086efb7bbb0005c60a5f
http://id.nii.ac.jp/1696/00005536/

Zobrazit plný text záznamu

境界層遷移の解明と制御研究会講演論文集第40回

Autor: Japan Aerospace Exploration Agency

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication.

境界層遷移の解明と制御研究会宇宙航空研究開発機構.東北大学流体科学研究所 20070313-20070316 宮崎日本
JAXA Workshop on Investigation and Control of Boundary-Layer Transition, Japan Aerospace Exploration Agen

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::807982888b553fea55fa8567c0cd714f
http://id.nii.ac.jp/1696/00005515/

Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání