Zobrazeno 1 - 10
of 21
pro vyhledávání: '"sweptback wing"'
Autor:
Jong-Seob Han, Christian Breitsamter
Publikováno v:
Applied Sciences, Vol 11, Iss 6, p 2450 (2021)
A sweptback angle can directly regulate a leading-edge vortex on various aerodynamic devices as well as on the wings of biological flyers, but the effect of a sweptback angle has not yet been sufficiently investigated. Here, we thoroughly investigate
Externí odkaz:
https://doaj.org/article/ce20bdb13a504fc9b919288880c1fc63
Autor:
Christian Breitsamter, Jong-Seob Han
Publikováno v:
Applied Sciences, Vol 11, Iss 2450, p 2450 (2021)
Applied Sciences
Volume 11
Issue 6
Applied Sciences
Volume 11
Issue 6
A sweptback angle can directly regulate a leading-edge vortex on various aerodynamic devices as well as on the wings of biological flyers, but the effect of a sweptback angle has not yet been sufficiently investigated. Here, we thoroughly investigate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f661814f24c84b4e8fce0c138fb7563f
https://www.mdpi.com/2076-3417/11/6/2450
https://www.mdpi.com/2076-3417/11/6/2450
Akademický článek
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Akademický článek
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Akademický článek
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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. :68-74
In this paper, a multi-objective design exploration for a three-element airfoil which consists of a slat, main wing, and flap was carried out by paying attention to the span wise flow effect. Reynolds Averaged Navier-Stokes Solver (RANS) was used for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::40168f4e73cab55c86a5c4a5e24fb981
http://id.nii.ac.jp/1696/00005612/
http://id.nii.ac.jp/1696/00005612/
Autor:
Herrmann, U.
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). :486-497
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
SST-CFD Workshop. International Workshops on Numer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::49d55beb78bf01e5b592ee07e24fabed
http://id.nii.ac.jp/1696/00005787/
http://id.nii.ac.jp/1696/00005787/
Autor:
Machida, Kentaro, Miyaji, Koji
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. :94-99
A 3D flutter of a sweptback wing is numerically investigated by coupling inviscid flow simulations with a bending-torsion beam structure model. The beam model of a 3D wing is a natural extension of a widely used 2D 2-degree-of-freedom structure model
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::63a3c540d7626207f86c0b15df5367f7
http://id.nii.ac.jp/1696/00006142/
http://id.nii.ac.jp/1696/00006142/
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33回・第34回 = JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :25-28
Development of point source disturbance in the three-dimensional boundary layer of yawed circular cylinders is studied using Direct Numerical Simulation (DNS). Using a 2D FFT technique, the waves are separated into two instability modes. One is the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::80517b3b6616a82cca96ce27e4bf64a0
http://id.nii.ac.jp/1696/00006556/
http://id.nii.ac.jp/1696/00006556/
Autor:
Ogoshi, Hirokage
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. :203-209
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
超音速航空機の翼に対する自然層流(NLF)の空力設計を3次元CFD(計算流体力学)および境界層安
National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan
超音速航空機の翼に対する自然層流(NLF)の空力設計を3次元CFD(計算流体力学)および境界層安
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::767331fcbad26894bbdf588ce9a24078
http://id.nii.ac.jp/1696/00041439/
http://id.nii.ac.jp/1696/00041439/