A Numerical Control Design Method for Prototypical Aeroelastic Wing Section with Structural Non-linearity

Baranyi, (2006) A Numerical Control Design Method for Prototypical Aeroelastic Wing Section with Structural Non-linearity.

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Item Type: Other
Subjects: Q Science > QA Mathematics and Computer Science > QA75 Electronic computers. Computer science / számítástechnika, számítógéptudomány
Divisions: 3D Internet-based Control and Communications Laboratory
Systems and Control Lab
Depositing User: Anna Karola Szemereki
Date Deposited: 11 Dec 2012 15:20
Last Modified: 11 Dec 2012 15:20
URI: http://eprints.sztaki.hu/id/eprint/4267

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