Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Benjamin L. Hinchliffe"'
Publikováno v:
AIAA Journal. 56:1541-1553
This paper presents an investigation of the influence of a nonconsistent approach in terms of mesh movement and mesh sensitivity calculation in a discrete adjoint-based optimization. Some mesh move...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::74bb6f0f022a165a1be204bb57b4a81a
https://doi.org/10.2514/1.j055904
https://doi.org/10.2514/1.j055904
Publikováno v:
AIAA Journal. 55:1140-1151
A method based on the Delaunay graph mapping mesh movement is proposed to eliminate mesh sensitivity, which is required in the discrete adjoint optimization framework. The method makes use of a one...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e08b3dda0e2bac837c691dcb45ab4207
https://doi.org/10.2514/1.j055212
https://doi.org/10.2514/1.j055212
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30e6b63c6a5c6fea808824601e155d13
https://doi.org/10.2514/6.2017-0461
https://doi.org/10.2514/6.2017-0461
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
A method based on the Delaunay graph mapping mesh movement is proposed to efficiently compute mesh sensitivity in the discrete adjoint optimisation framework. The method results in a one-to-one explicit algebraic mapping between the volume and surfac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c0cf5769b40a2c320263c8ebfe7160c9
https://doi.org/10.2514/6.2016-0291
https://doi.org/10.2514/6.2016-0291
Autor:
Ning Qin, Benjamin L. Hinchliffe
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Shock control bumps are a promising device for improving the aerodynamic efficiency of transonic aircraft. From the literature, the peak location and bump height are the most sensitive parameters, therefore the deployment position and size of the sho
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::619cf6cfbd96c215dd0856b3bd4f1b46
https://doi.org/10.2514/6.2016-0560
https://doi.org/10.2514/6.2016-0560
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Shock control bumps are a promising device for improving the aerodynamic efficiency of high subsonic aircraft. From the previous research, the peak location and bump height are the most sensitive parameters, therefore the deployment position and size
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0cd162ca8a6ff546641f9bbf0974c3bb
https://doi.org/10.2514/6.2015-1488
https://doi.org/10.2514/6.2015-1488