Zobrazeno 1 - 10
of 128 351
pro vyhledávání: '"Airfoil"'
Autor:
Wang, Dian1 (AUTHOR), Cai, Chang2,3 (AUTHOR) caichang@iet.cn, Zha, Rongyu1 (AUTHOR), Peng, Chaoyi4 (AUTHOR), Feng, Xuebin4 (AUTHOR), Liang, Pengcheng4 (AUTHOR), Meng, Keqilao5 (AUTHOR), Kou, Jianyu6 (AUTHOR), Maeda, Takao7 (AUTHOR), Li, Qing'an2,3,8 (AUTHOR) caichang@iet.cn
Publikováno v:
Energies (19961073). Nov2024, Vol. 17 Issue 21, p5518. 17p.
Autor:
Wang, Xu1,2 (AUTHOR) ocotea@163.com, Qian, Weiqi1 (AUTHOR) qwqhyy2024@163.com, Zhao, Tun1 (AUTHOR) leiluodelei@nudt.edu.cn, He, Lei1 (AUTHOR) chenhai@mail.nwpu.edu.cn, Chen, Hai1 (AUTHOR) engineercui@163.com, Sun, Haisheng3 (AUTHOR), Tian, Yuan2 (AUTHOR), Cui, Jinlei1 (AUTHOR)
Publikováno v:
Symmetry (20738994). Jul2024, Vol. 16 Issue 7, p791. 17p.
Autor:
Sang, Le Quang1,2 (AUTHOR) lehang212@gmail.com, Phengpom, Tinnapob3 (AUTHOR), Thin, Dinh Van4 (AUTHOR) thindv@epu.edu.vn, Duc, Nguyen Huu4 (AUTHOR) ducnh@epu.edu.vn, Hang, Le Thi Thuy1 (AUTHOR), Huyen, Cu Thi Thanh1 (AUTHOR), Huong, Nguyen Thi Thu1 (AUTHOR), Tran, Quynh T.1,5 (AUTHOR) ducnh@epu.edu.vn
Publikováno v:
Energies (19961073). Aug2024, Vol. 17 Issue 16, p4113. 19p.
Publikováno v:
International Journal of Vehicle Structures & Systems (IJVSS). 2024, Vol. 16 Issue 1, p94-97. 4p.
Autor:
Sesalim, Dean1 (AUTHOR) dsesalim@swin.edu.au, Naser, Jamal1 (AUTHOR) dsesalim@swin.edu.au
Publikováno v:
Energies (19961073). Jun2024, Vol. 17 Issue 11, p2768. 17p.
Autor:
Feraru, Mădălin-Dorin1 (AUTHOR) dorin.feraru@stud.aero.upb.ro, Măriuța, Daniel2 (AUTHOR) daniel.mariuta@mta.ro, Stoia-Djeska, Marius1 (AUTHOR) marius.stoia@upb.ro, Grigorie, Lucian-Teodor1 (AUTHOR) teodor.grigorie@upb.ro
Publikováno v:
Biomimetics (2313-7673). Oct2024, Vol. 9 Issue 10, p635. 18p.
This study presents wall-resolved large-eddy simulations (WRLES) of a high-lift airfoil, based on high-order flux reconstruction (FR) commercial software Dimaxer, which runs on consumer level GPUs. A series of independence tests are conducted, includ
Externí odkaz:
http://arxiv.org/abs/2411.05686
The flow over a NACA0012 airfoil at a moderate Reynolds number Re = 50,000 and angle of attack of alpha = 3 degrees is investigated using the lattice-Boltzmann method (LBM). The LBM solutions are computed in direct numerical simulation (DNS) mode, i.
Externí odkaz:
http://arxiv.org/abs/2411.04763