<?xml version="1.0" encoding="UTF-8"?>
<collection xmlns="http://www.loc.gov/MARC21/slim">
 <record>
  <leader>     caa a22        4500</leader>
  <controlfield tag="001">463244176</controlfield>
  <controlfield tag="003">CHVBK</controlfield>
  <controlfield tag="005">20180405153321.0</controlfield>
  <controlfield tag="007">cr unu---uuuuu</controlfield>
  <controlfield tag="008">170326e20070301xx      s     000 0 eng  </controlfield>
  <datafield tag="024" ind1="7" ind2="0">
   <subfield code="a">10.1007/s00158-006-0064-4</subfield>
   <subfield code="2">doi</subfield>
  </datafield>
  <datafield tag="035" ind1=" " ind2=" ">
   <subfield code="a">(NATIONALLICENCE)springer-10.1007/s00158-006-0064-4</subfield>
  </datafield>
  <datafield tag="100" ind1="1" ind2=" ">
   <subfield code="a">Kobelev</subfield>
   <subfield code="D">V.</subfield>
   <subfield code="u">Fachbereich 11, PB A203, Institut für Mechanik und Regelungstechnik-Mechatronik, Paul-Bonatz-Str. 9-11, 57068, Siegen, Germany</subfield>
   <subfield code="4">aut</subfield>
  </datafield>
  <datafield tag="245" ind1="1" ind2="0">
   <subfield code="a">Sensitivity analysis of the linear nonconservative systems with fractional damping</subfield>
   <subfield code="h">[Elektronische Daten]</subfield>
   <subfield code="c">[V. Kobelev]</subfield>
  </datafield>
  <datafield tag="520" ind1="3" ind2=" ">
   <subfield code="a">In this paper, the influence of small structural perturbation on a linear, nonconservative dynamical system exhibiting fractional bifurcation was investigated. In considering design problems for nonconservative systems, the integral structural characteristics as fundamental frequencies, critical loads for instability, and the sensitivity analysis play an important part. In this paper, the influence of small perturbation on a linear, nonconservative dynamical system exhibiting a flutter type bifurcation was investigated. The hereditary damping is described by means of fractional derivatives. To study the dynamical instability for nonconservative governing equations with fractional damping, the method of auxiliary eigenvalue problem is applied. The stability conditions of generalized Lyapunov type for the system with hereditary damping were derived. A new analytical framework for the coupled optimization of aero-structural, fractionally damped systems is presented. The approach to obtain aerodynamic sensitivities is based on adjoint systems.</subfield>
  </datafield>
  <datafield tag="540" ind1=" " ind2=" ">
   <subfield code="a">Springer-Verlag Berlin Heidelberg, 2006</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Nonconservative systems</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Fractional damping</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="773" ind1="0" ind2=" ">
   <subfield code="t">Structural and Multidisciplinary Optimization</subfield>
   <subfield code="d">Springer-Verlag</subfield>
   <subfield code="g">33/3(2007-03-01), 179-188</subfield>
   <subfield code="x">1615-147X</subfield>
   <subfield code="q">33:3&lt;179</subfield>
   <subfield code="1">2007</subfield>
   <subfield code="2">33</subfield>
   <subfield code="o">158</subfield>
  </datafield>
  <datafield tag="856" ind1="4" ind2="0">
   <subfield code="u">https://doi.org/10.1007/s00158-006-0064-4</subfield>
   <subfield code="q">text/html</subfield>
   <subfield code="z">Onlinezugriff via DOI</subfield>
  </datafield>
  <datafield tag="908" ind1=" " ind2=" ">
   <subfield code="D">1</subfield>
   <subfield code="a">research-article</subfield>
   <subfield code="2">jats</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">856</subfield>
   <subfield code="E">40</subfield>
   <subfield code="u">https://doi.org/10.1007/s00158-006-0064-4</subfield>
   <subfield code="q">text/html</subfield>
   <subfield code="z">Onlinezugriff via DOI</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">100</subfield>
   <subfield code="E">1-</subfield>
   <subfield code="a">Kobelev</subfield>
   <subfield code="D">V.</subfield>
   <subfield code="u">Fachbereich 11, PB A203, Institut für Mechanik und Regelungstechnik-Mechatronik, Paul-Bonatz-Str. 9-11, 57068, Siegen, Germany</subfield>
   <subfield code="4">aut</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">773</subfield>
   <subfield code="E">0-</subfield>
   <subfield code="t">Structural and Multidisciplinary Optimization</subfield>
   <subfield code="d">Springer-Verlag</subfield>
   <subfield code="g">33/3(2007-03-01), 179-188</subfield>
   <subfield code="x">1615-147X</subfield>
   <subfield code="q">33:3&lt;179</subfield>
   <subfield code="1">2007</subfield>
   <subfield code="2">33</subfield>
   <subfield code="o">158</subfield>
  </datafield>
  <datafield tag="900" ind1=" " ind2="7">
   <subfield code="a">Metadata rights reserved</subfield>
   <subfield code="b">Springer special CC-BY-NC licence</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="898" ind1=" " ind2=" ">
   <subfield code="a">BK010053</subfield>
   <subfield code="b">XK010053</subfield>
   <subfield code="c">XK010000</subfield>
  </datafield>
  <datafield tag="949" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="F">NATIONALLICENCE</subfield>
   <subfield code="b">NL-springer</subfield>
  </datafield>
 </record>
</collection>
