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1.	Original version of the author's contribution in proceedings, page 606, section DYN.: PDF STABILITY MARGINS EXPERIMENTAL SEARCH OF AN AEROELASTIC SYSTEM Malínek, P. Aircraft developers and builders commonly design and produce potentially unstable aeroelastic systems. Detailed and reliable knowledge of real dynamic properties of the s [...] Detailed record - Similar records
2.	Original version of the author's contribution as presented on CD, , page 77. : PDF Direct dynamic response computation of an aircraft structure based on experimentally identified modal model Malínek, P. Detailed record - Similar records

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