Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Kaichun, Zeng"'
Publikováno v:
Applied Sciences, Vol 13, Iss 21, p 12077 (2023)
To address the contradiction between the convergence error and convergence rate in the LMS algorithm, this study proposes a variable-step-size adaptive filter algorithm with a momentum term based on the logistic function. First, the normalization LMS
Externí odkaz:
https://doaj.org/article/3907036f45204911bdb59f3bd685e9c7
Publikováno v:
Shock and Vibration, Vol 2021 (2021)
The static aeroelastic behaviours of a flat-plate forward-swept wing model in the vicinity of static divergence are investigated by numerical simulations and wind tunnel tests. A medium fidelity model based on the vortex lattice method (VLM) and nonl
Externí odkaz:
https://doaj.org/article/984140152d6b43ba98d2277097a977fd
Publikováno v:
Chinese Journal of Aeronautics. 36:58-75
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::707e775d77046e5a75307214647ee9aa
https://doi.org/10.1016/j.cja.2022.07.017
https://doi.org/10.1016/j.cja.2022.07.017
Underconstrained Cable-Driven Parallel Suspension System of Virtual Flight Test Model in Wind Tunnel
Publikováno v:
Computer Modeling in Engineering & Sciences. 135:395-416
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::01119878cabe3a378d3d1cd022a9c7f6
https://doi.org/10.32604/cmes.2022.021650
https://doi.org/10.32604/cmes.2022.021650
Publikováno v:
Computer Modeling in Engineering & Sciences. 133:1-29
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f9d7b3aba30ab998b942e62c3ce2813e
https://doi.org/10.32604/cmes.2022.020572
https://doi.org/10.32604/cmes.2022.020572
Publikováno v:
In Chinese Journal of Aeronautics August 2013 26(4):831-840
Autor:
Jinwu Xiang, Kaichun Zeng
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A framework for modeling of the flexible air-breathing hypersonic vehicles (HSVs) with nonuniform fuselage section is developed and the effects of nonuniformities on flight dynamics are investigated. The flexible fuselage is modeled as a free-free be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c083ab1bf8ed8d5ef1922cb9716e0c4a
https://doi.org/10.2514/6.2013-1722
https://doi.org/10.2514/6.2013-1722