NUMERICAL APPROACH IN AEROELASTICITY
Aircraft wing design processes should comprise specific analyses oriented towards aeroelasticity, which is one of the essential factors determining flight envelope boundaries. For such cases, static or dynamic aeroelastic phenomena can be simulated using CFD simulation software. ANSYS software offe...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Silesian University of Technology
2016-12-01
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| Series: | Scientific Journal of Silesian University of Technology. Series Transport |
| Subjects: | |
| Online Access: | http://sjsutst.polsl.pl/archives/2016/vol93/115_SJSUTST93_2016_SlobodaKorbaHovanecPila.pdf |
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| _version_ | 1846095895338156032 |
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| author | Oskar SLOBODA Peter KORBA Michal HOVANEC Jan PILA |
| author_facet | Oskar SLOBODA Peter KORBA Michal HOVANEC Jan PILA |
| author_sort | Oskar SLOBODA |
| collection | DOAJ |
| description | Aircraft wing design processes should comprise specific analyses
oriented towards aeroelasticity, which is one of the essential factors determining flight envelope boundaries. For such cases, static or dynamic aeroelastic phenomena can be simulated using CFD simulation software. ANSYS software offers the fluid structure interaction (FSI) method for solving this multiphysics problem |
| format | Article |
| id | doaj-art-d8ab8fdb05134a819550d4f4a4f089b6 |
| institution | Kabale University |
| issn | 0209-3324 2450-1549 |
| language | English |
| publishDate | 2016-12-01 |
| publisher | Silesian University of Technology |
| record_format | Article |
| series | Scientific Journal of Silesian University of Technology. Series Transport |
| spelling | doaj-art-d8ab8fdb05134a819550d4f4a4f089b62025-01-02T09:06:01ZengSilesian University of TechnologyScientific Journal of Silesian University of Technology. Series Transport0209-33242450-15492016-12-019311512210.20858/sjsutst.2016.93.12NUMERICAL APPROACH IN AEROELASTICITYOskar SLOBODAPeter KORBAMichal HOVANECJan PILAAircraft wing design processes should comprise specific analyses oriented towards aeroelasticity, which is one of the essential factors determining flight envelope boundaries. For such cases, static or dynamic aeroelastic phenomena can be simulated using CFD simulation software. ANSYS software offers the fluid structure interaction (FSI) method for solving this multiphysics problemhttp://sjsutst.polsl.pl/archives/2016/vol93/115_SJSUTST93_2016_SlobodaKorbaHovanecPila.pdfaeroelasticityfluid structure interactionwing |
| spellingShingle | Oskar SLOBODA Peter KORBA Michal HOVANEC Jan PILA NUMERICAL APPROACH IN AEROELASTICITY Scientific Journal of Silesian University of Technology. Series Transport aeroelasticity fluid structure interaction wing |
| title | NUMERICAL APPROACH IN AEROELASTICITY |
| title_full | NUMERICAL APPROACH IN AEROELASTICITY |
| title_fullStr | NUMERICAL APPROACH IN AEROELASTICITY |
| title_full_unstemmed | NUMERICAL APPROACH IN AEROELASTICITY |
| title_short | NUMERICAL APPROACH IN AEROELASTICITY |
| title_sort | numerical approach in aeroelasticity |
| topic | aeroelasticity fluid structure interaction wing |
| url | http://sjsutst.polsl.pl/archives/2016/vol93/115_SJSUTST93_2016_SlobodaKorbaHovanecPila.pdf |
| work_keys_str_mv | AT oskarsloboda numericalapproachinaeroelasticity AT peterkorba numericalapproachinaeroelasticity AT michalhovanec numericalapproachinaeroelasticity AT janpila numericalapproachinaeroelasticity |