Zobrazeno 1 - 10
of 49
pro vyhledávání: '"high angle of attack aerodynamics"'
Publikováno v:
Aerospace, Vol 10, Iss 9, p 746 (2023)
This paper introduces a generic model for the study of aerodynamic behaviour relevant to fifth-generation high-performance aircraft. The model design is presented, outlining simplifications made to retain the key features of modern high-performance v
Externí odkaz:
https://doaj.org/article/8add2cf1ec6f4334b972047f4ca2282a
Akademický článek
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Akademický článek
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Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1245:1-13
ボルテックス･フラップ付きデルタ翼の後退角の変化が空力特性に及ぼす影響を調べるために、後退角70度のボルテックス･フラップ付きデルタ翼模型を用いて風洞実験を行った。空気
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::69847808c9992f5fd937622950096216
http://id.nii.ac.jp/1696/00041216/
http://id.nii.ac.jp/1696/00041216/
Autor:
Miroslav Mokry
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
42nd AIAA Aerospace Sciences Meeting & Exhibit (from 1/5/2004 to 1/8/2004), Reno, Nevada
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Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0e9171f1c6ba74dc2a5b6810f3a26e95
https://doi.org/10.2514/6.2004-606
https://doi.org/10.2514/6.2004-606
Autor:
Petterson, Kristian
High angle-of-attack aerodynamics has been the focus of much attention as a result of the drive to increase combat aircraft manoeuverability and thereby improve survivability. A key factor in this regime is the behaviour of the complex vortical wake
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od________70::a0d01c946b363fcee37a1858c9ed1e34
https://dspace.lib.cranfield.ac.uk/handle/1826/18584
https://dspace.lib.cranfield.ac.uk/handle/1826/18584
Autor:
Alkhozam, Abdullah M.
A flow visualization study of the vortical flow over a cropped double-delta wing model with sharp leading edges and its three derivatives with small geometric modifications (fillets) at the strake wing junction was conducted in the Naval Postgraduate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::987f2fb6cadad1b3545ec6dee8dcfee3
https://hdl.handle.net/10945/30867
https://hdl.handle.net/10945/30867
Autor:
Li, Feng-Hsi
A water tunnel flow visualization was performed to study the vortex development and bursting phenomena on a baseline double delta wing model and a modified double delta wing model. The primary focus of this study was two-fold: First, to study the sta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::8d22cba26ebe6d1eb24e7f8209b4caa5
https://hdl.handle.net/10945/23777
https://hdl.handle.net/10945/23777
Autor:
Kim, Chang Ho.
A water tunnel flow visualization investigation was performed to study the vortex development and bursting phenomena on a 2.3 % scale model of a X-31A-Like fighter aircraft. The main focus of this study was two-fold : First, to study the effects of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::3899f9689e987a1abfdd4dfe285fab10
https://hdl.handle.net/10945/26553
https://hdl.handle.net/10945/26553
Autor:
Frink, William D., Jr.
A low-speed wind tunnel investigation was conducted to examine the vortex wake downstream of a three-percent scale model of the YF-17 lightweight fighter prototype at high angles of attack. The study was in support of NASA ames Research Center's wind
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::082ee72c68cc169e1489d16096998ad1
https://hdl.handle.net/10945/27586
https://hdl.handle.net/10945/27586