Zobrazeno 1 - 10
of 24
pro vyhledávání: '"Mohagna J. Pandya"'
Autor:
Michael D. Bozeman, Mohagna J. Pandya
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45f178fcaeb3c646d48489d0efdb3f75
https://doi.org/10.2514/6.2023-1759
https://doi.org/10.2514/6.2023-1759
Publikováno v:
AIAA Journal. 59:4719-4738
The unstructured-grid mixed-element cell-centered finite-volume flow solver USM3D is enhanced for massively parallel computations. The paper describes modifications to the flow solver and paralleli...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a70cab25c1ff7ba70218b1ef2fda761d
https://doi.org/10.2514/1.j060064
https://doi.org/10.2514/1.j060064
Publikováno v:
AIAA Journal. :1-15
The unstructured mixed-element cell-centered finite volume flow solver USM3D is enhanced with new capabilities such as line generation for general unstructured grids and optimization of the iterati...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0c10e3c33c629d10d13620c1eb25298f
https://doi.org/10.2514/1.j059720
https://doi.org/10.2514/1.j059720
Autor:
Boris Diskin, Li Wang, Nashat N. Ahmad, Yi Liu, Stephen L. Wood, William K. Anderson, Hiroaki Nishikawa, Christopher L. Rumsey, Mohagna J. Pandya, Marshall C. Galbraith, Joseph M. Derlaga
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d81ef002c8cf54926468c22aaa6d6d95
https://doi.org/10.2514/6.2021-1552.c1
https://doi.org/10.2514/6.2021-1552.c1
Autor:
Stephen L. Wood, Hiroaki Nishikawa, Christopher L. Rumsey, Yi Liu, Mohagna J. Pandya, Joseph M. Derlaga, Li Wang, William K. Anderson, Nashat N. Ahmad, Boris Diskin, Marshall C. Galbraith
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f497c754dccd3b04e34b5ebe9bed087f
https://doi.org/10.2514/6.2021-1552
https://doi.org/10.2514/6.2021-1552
Publikováno v:
AIAA Journal. 55:3409-3424
Enhancements to the previously reported hierarchical adaptive nonlinear iteration methods implemented in a mixed-element cell-centered framework have been made to improve robustness, efficiency, an...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6388ee9b9457296673db4c5cffaa3b27
https://doi.org/10.2514/1.j055823
https://doi.org/10.2514/1.j055823
Publikováno v:
AIAA Scitech 2019 Forum.
The unstructured, mixed-element, cell-centered, finite-volume flow solver USM3D is enhanced with new capabilities including parallelization, line generation for general unstructured grids, improved discretization scheme, and optimized iterative solve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3bb5d842f058303ff66c20379da8404
https://doi.org/10.2514/6.2019-2333
https://doi.org/10.2514/6.2019-2333
Publikováno v:
AIAA Journal. 54:2589-2610
Several improvements to the mixed-element USM3D discretization and defect-correction schemes have been made. A new methodology for nonlinear iterations, called the Hierarchical Adaptive Nonlinear Iteration Method, has been developed and implemented.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::efc48a118423162da36407afa3b5eb75
https://doi.org/10.2514/1.j054545
https://doi.org/10.2514/1.j054545
Autor:
Mohagna J. Pandya, James L. Thomas, William K. Anderson, Christopher L. Rumsey, Yi Liu, Boris Diskin, Hiroaki Nishikawa
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Grid convergence studies are performed to establish reference solutions for benchmark three dimensional turbulent flows in support of the ongoing turbulence model verification and validation e ort at the Turbulence Modeling Resource website curated b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9d5dca435f7ccd839a0e50bdfbc9da01
https://doi.org/10.2514/6.2018-1102
https://doi.org/10.2514/6.2018-1102
Publikováno v:
Journal of Aircraft. 50:1682-1695
Turbulent flow computations of the NASA “trap-wing” high-lift configuration are performed at various angles of attack using a k-ω family of models to assess their capabilities for high-lift design and optimization applications. The four k-ω mod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad1d1e0fc2594f21c17bcfdc78998d3e
https://doi.org/10.2514/1.c031492
https://doi.org/10.2514/1.c031492