000 02910nam a22004815i 4500
001 978-3-642-36552-2
003 DE-He213
005 20140220082905.0
007 cr nn 008mamaa
008 130324s2013 gw | s |||| 0|eng d
020 _a9783642365522
_9978-3-642-36552-2
024 7 _a10.1007/978-3-642-36552-2
_2doi
050 4 _aTA355
050 4 _aTA352-356
072 7 _aTGMD4
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aSCI018000
_2bisacsh
082 0 4 _a620
_223
100 1 _aSpelsberg-Korspeter, Gottfried.
_eauthor.
245 1 0 _aRobust Structural Design against Self-Excited Vibrations
_h[electronic resource] /
_cby Gottfried Spelsberg-Korspeter.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg :
_bImprint: Springer,
_c2013.
300 _aVI, 100 p. 44 illus., 32 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringerBriefs in Applied Sciences and Technology,
_x2191-530X
505 0 _aPerturbation of a linear conservative system by periodic parametric excitation -- Eigenvalue placement for structural optimization -- Passive stabilization of discrete systems -- Passive stabilization in continuous systems -- Structural optimization of a disk brake -- Nonlinear analysis of systems under periodic parametric excitation.
520 _aThis book studies methods for a robust design of rotors against self-excited vibrations. The occurrence of self-excited vibrations in engineering applications if often unwanted and in many cases difficult to model. Thinking of complex systems such as machines with many components and mechanical contacts, it is important to have guidelines for design so that the functionality is robust against small imperfections. This book discusses the question on how to design a structure such that unwanted self-excited vibrations do not occur. It shows theoretically and practically that the old design rule to avoid multiple eigenvalues points toward the right direction and have optimized structures accordingly. This extends results for the well-known flutter problem in which equations of motion with constant coefficients occur to the case of a linear conservative system with arbitrary time periodic perturbations.
650 0 _aEngineering.
650 0 _aVibration.
650 0 _aEngineering design.
650 1 4 _aEngineering.
650 2 4 _aVibration, Dynamical Systems, Control.
650 2 4 _aEngineering Design.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783642365515
830 0 _aSpringerBriefs in Applied Sciences and Technology,
_x2191-530X
856 4 0 _uhttp://dx.doi.org/10.1007/978-3-642-36552-2
912 _aZDB-2-ENG
999 _c97900
_d97900