Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Takanashi's method"'
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 34:101-106
航空宇宙技術研究所 6-7 JUN. 1996 東京 日本
National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan
遷音速時において目標圧力分布を有する翼形状を計算するための高梨法は大アスペクト比の翼
National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan
遷音速時において目標圧力分布を有する翼形状を計算するための高梨法は大アスペクト比の翼
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::6ce477d7197556c63760b0fb69dcfd8d
http://id.nii.ac.jp/1696/00036872/
http://id.nii.ac.jp/1696/00036872/
Autor:
Bartelheimer, Wolf
Publikováno v:
Inverse Problems in Science and Engineering; November 1996, Vol. 4 Issue: 1 p21-51, 31p
Autor:
Nili-Ahmadabadi, Mahdi1 (AUTHOR) nili@mech.sharif.edu, Durali, Mohammad2 (AUTHOR), Hajilouy-Benisi, Ali1 (AUTHOR), Ghadak, Farhad3 (AUTHOR)
Publikováno v:
Inverse Problems in Science & Engineering. Dec2009, Vol. 17 Issue 8, p1037-1057. 21p. 3 Diagrams, 2 Charts, 18 Graphs.
Publikováno v:
Aircraft Engineering & Aerospace Technology; 2019, Vol. 91 Issue 1, p124-133, 10p
Autor:
Streit, T., Hoffrogge, C.
Publikováno v:
Aeronautical Journal; Nov2017, Vol. 121 Issue 1245, p1733-1757, 25p
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. :166-171
In this article, it is shown that the design of a new airfoil can be performed on an ordinary Personal Computer. A software system consisting of Computational Fluid Dynamics and Graphical User Interface programs has been developed to be an aerodynami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::44609bacb4aec316568da3d201e420e9
http://id.nii.ac.jp/1696/00006625/
http://id.nii.ac.jp/1696/00006625/
Autor:
Wolf Bartelheimer
Publikováno v:
Inverse Problems in Engineering. 4:21-51
A design method for transonic airfoils and wings based on the solution of the Euler/Navier-Stokes equations is described. The applied design strategy is an inverse design method based on the work of Takanashi. The difference between the computed pres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5579f3e504b59325e819c8687a7220e7
https://doi.org/10.1080/174159796088027632
https://doi.org/10.1080/174159796088027632
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 44:241-243
航空宇宙技術研究所 16-18 Jun. 1999 東京 日本
National Aerospace Laboratory 16-18 Jun. 1999 Tokyo Japan
非構造格子法を用いて、高梨の逆設計法を翼-ナセル形態に拡張した。翼-ナセル形態の周囲
National Aerospace Laboratory 16-18 Jun. 1999 Tokyo Japan
非構造格子法を用いて、高梨の逆設計法を翼-ナセル形態に拡張した。翼-ナセル形態の周囲
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::055987e6e4901ff6490c1285b15a7469
http://id.nii.ac.jp/1696/00037464/
http://id.nii.ac.jp/1696/00037464/
Autor:
Wolf Bartelheimer
A design method for transonic airfoils and wings based on the solution of the Euler-/Navier-Stokes equations is described. The applied design strategy is an inverse design method based on the work of Takanashi. The difference between the computed pre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4aaa62f0f3fdc32447cc27396901cd6d
https://elib.dlr.de/36371/
https://elib.dlr.de/36371/
Polymer Gears discusses polymer gear design and their efficient mechanical properties, light weight, and low noise during operation. As plastic gears are replacing metallic gears in traditional and new applications, there is still lack of material ch