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COMAT 2006 >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/123456789/1052
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| Title: | STRUCTURAL MODELLING BY MBS METHOD APPLIED TO LINKAGES USED TO AILERON AIRCRAFT CONTROL |
| Authors: | GHITESCU, Marius |
| Keywords: | mechanical systems
multibody systems
structural modeling
kinematic analysis
aircraft
Flaps |
| Issue Date: | Oct-2006 |
| Publisher: | Transilvania University Press of Braşov |
| Citation: | GOOGLE SCHOLAR |
| Series/Report no.: | COMAT 2006;1-7 |
| 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 concrete mechanical systems. This will be the bases for dynamic modelling of these subsystems as parts of the whole product (airplane). |
| URI: | http://hdl.handle.net/123456789/1052 |
| ISBN: | 973 - 635 - 823 - 2 |
| Appears in Collections: | COMAT 2006
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