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DSpace at Transilvania University >
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COMEC 2005 >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/123456789/828
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| Title: | STRUCTURAL MODELING BY MBS METHOD APPLIED TO LINKAGES USED TO FLAPS AIRCRAFT CONTROL |
| Authors: | GHITESCU, Marius
VISA, Ion |
| Keywords: | mechanical systems
multibody systems
structural modeling
kinematic analysis
aircraft
Flaps |
| Issue Date: | Oct-2005 |
| Publisher: | Transilvania University Press of Braşov |
| Citation: | GOOGLE SCHOLAR |
| Series/Report no.: | COMEC 2005;1-6 |
| Abstract: | The aim of the paper is structural modelling of linkages used in airplane flaps control, on bases of the Multibody System method (MBS). In virtual prototyping of the aircraft , these linkages have to be modeled by a minimum number of bodies (MBS min). In the paper an appropiate algorithm is descriebed and also applied for six concrete mechanical systems. This will be the bases for kinematic and dynamic modelling of these subsystems as parts of the whole product (airplane). |
| URI: | http://hdl.handle.net/123456789/828 |
| ISBN: | 973 - 635 - 593 – 4 |
| Appears in Collections: | COMEC 2005
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