Zobrazeno 1 - 10
of 58
pro vyhledávání: '"Shufang SONG"'
Publikováno v:
气体物理, Vol 9, Iss 4, Pp 39-55 (2024)
The accurate prediction of aerothermal loads is the basis to guide hypersonic vehicle design. Under the background that classical aerothermal prediction methods are more and more difficult to meet the demand of efficient and accurate aerothermal pred
Externí odkaz:
https://doaj.org/article/018261b8be454bb79e640d026b830f13
Publikováno v:
International Journal of Aerospace Engineering, Vol 2022 (2022)
Aero-engine is known as the heart of an aircraft. Fatigue is one of the main causes of aero-engine failure, therefore, it is essential to predict the fatigue life in the aero-engine design process. Due to the uncertainty of influencing factors, it is
Externí odkaz:
https://doaj.org/article/0ec57b5f3e2c41e8afa512e275baaff7
Publikováno v:
Mathematics, Vol 9, Iss 19, p 2489 (2021)
For multidimensional dependent cases with incomplete probability information of random variables, global sensitivity analysis (GSA) theory is not yet mature. The joint probability density function (PDF) of multidimensional variables is usually unknow
Externí odkaz:
https://doaj.org/article/bfbbbbb459f94a0aba55bcb261e83318
Autor:
Shufang Song, Lu Wang
Publikováno v:
Symmetry, Vol 13, Iss 1, p 90 (2021)
Global sensitivity analysis (GSA) is a useful tool to evaluate the influence of input variables in the whole distribution range. Variance-based methods and moment-independent methods are widely studied and popular GSA techniques despite their several
Externí odkaz:
https://doaj.org/article/b15ab5f3da654df18024c3ee6747ee98
Publikováno v:
International Journal of Aerospace Engineering, Vol 2017 (2017)
Airfoil geometric uncertainty can generate aerodynamic characteristics fluctuations. Uncertainty quantification is applied to compute its impact on the aerodynamic characteristics. In addition, the contribution of each uncertainty variable to aerodyn
Externí odkaz:
https://doaj.org/article/6eb5e11ade514d16b9f7c46d7a9f6f04
Publikováno v:
Medicine; 6/21/2024, Vol. 103 Issue 25, p1-7, 7p
Publikováno v:
Environmental Science and Pollution Research. 30:46869-46883
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0efdf0b005eb49cae2276cc76eb252ad
https://doi.org/10.1007/s11356-023-25646-w
https://doi.org/10.1007/s11356-023-25646-w
Publikováno v:
Photodiagnosis and Photodynamic Therapy. 42:103336
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22ce31470e271d7180314d5086d16061
https://doi.org/10.1016/j.pdpdt.2023.103336
https://doi.org/10.1016/j.pdpdt.2023.103336
Publikováno v:
Acta Mechanica Sinica. 37:1416-1432
Adjoint method is widely used in aerodynamic design because only once solution of flow field is required for adjoint method to obtain the gradients of all design variables. However, the calculation cost of adjoint vector is approximately equal to tha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a77cb8702ca6189e572a70d760c3b7fa
https://doi.org/10.1007/s10409-021-01119-6
https://doi.org/10.1007/s10409-021-01119-6
Publikováno v:
Computer Modeling in Engineering & Sciences. 128:65-85
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8096dedb97cb897951a72625570f91a6
https://doi.org/10.32604/cmes.2021.015378
https://doi.org/10.32604/cmes.2021.015378