LEADER 00880nam0-22003131i-450- 001 990000481770403321 005 20080421122112.0 035 $a000048177 035 $aFED01000048177 035 $a(Aleph)000048177FED01 035 $a000048177 100 $a20020821d1965----km-y0itay50------ba 101 0 $aeng 105 $aa-------001yy 200 1 $a<>survey of modern algebra$fGarrett Birkhoff, Saunders Mac Lane 205 $a3rd ed. 210 $aNew York$cMac Millan C.$dİ1965 215 $a437 p.$cill.$d24 cm 610 0 $aAlgebra moderna 676 $a516 700 1$aBirkhoff,$bGarrett$f<1911-1996>$013068 701 1$aMac Lane,$bSaunders$026298 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990000481770403321 952 $a10 B II 83$b6498$fDINEL 959 $aDINEL 996 $aSurvey of modern algebra$9332279 997 $aUNINA LEADER 00891nam0-2200325---450- 001 990008672410403321 005 20080612115313.0 010 $a978-88-7487-213-8 035 $a000867241 035 $aFED01000867241 035 $a(Aleph)000867241FED01 035 $a000867241 100 $a20080612d2007----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $a--------001cy 200 1 $a<>rito$ein psicologia, in patologia, in terapia$fa cura di Claudio Widmann 210 $aRoma$cMagi$dİ2007 215 $a310 p.$d22 cm 225 1 $aImmagini dall'inconscio 610 0 $aRito$aInterpretazione psicanalitica 676 $a150.195 4$v21$zita 702 1$aWidmann,$bClaudio 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008672410403321 952 $a150.19 WID 1$b3781$fBFS 959 $aBFS 996 $aRito$9718111 997 $aUNINA LEADER 04267nam 2200709 450 001 9910809416003321 005 20210515003044.0 010 $a1-68015-770-1 010 $a3-11-038945-2 010 $a3-11-033837-8 024 7 $a10.1515/9783110338379 035 $a(CKB)3360000000515109 035 $a(EBL)1663201 035 $a(SSID)ssj0001401337 035 $a(PQKBManifestationID)11890561 035 $a(PQKBTitleCode)TC0001401337 035 $a(PQKBWorkID)11344673 035 $a(PQKB)10963062 035 $a(MiAaPQ)EBC1663201 035 $a(DE-B1597)214658 035 $a(OCoLC)898769809 035 $a(DE-B1597)9783110338379 035 $a(Au-PeEL)EBL1663201 035 $a(CaPaEBR)ebr11010283 035 $a(CaONFJC)MIL808095 035 $a(PPN)187994501 035 $a(EXLCZ)993360000000515109 100 $a20150204h20152015 uy 0 101 0 $aeng 135 $aurun#---|u||u 181 $ctxt 182 $cc 183 $acr 200 10$aAeroelastic vibrations and stability of plates and shells /$fSergey D. Algazin, Igor A. Kijko 210 1$aBerlin, Germany :$cDe Gruyter,$d2015. 210 4$dİ2015 215 $a1 online resource (234 p.) 225 1 $aDe Gruyter Studies in Mathematical Physics,$x2194-3532 ;$vVolume 25 300 $aDescription based upon print version of record. 311 $a3-11-040491-5 311 $a3-11-033836-X 320 $aIncludes bibliographical references. 327 $tFront matter --$tPreface --$tContents --$tIntroduction --$t1. Statement of the problem --$t2. Determination of aerodynamic pressure --$t3. Mathematical statement of problems --$t4. Reduction to a problem on a disk --$t5. Test problems --$t6. Rectangular plate --$t7. Flutter of a rectangular plate of variable stiffness or thickness --$t8. Viscoelastic plates --$t9. General formulation --$t10. Determination of aerodynamic pressure --$t11. The shallow shell as part of an airfoil --$t12. The shallow shell of revolution --$t13. The conical shell: external flow --$t14. The conical shell: internal flow --$t15. Example calculations --$t16. Discretization of the Laplace operator --$t17. Discretization of linear equations in mathematical physics with separable variables --$t18. Eigenvalues and eigenfunctions of the Laplace operator --$t19. Eigenvalues and eigenfunctions of a biharmonic operator --$t20. Eigenvalues and eigenfunctions of the Laplace operator on an arbitrary domain --$t21. Eigenvalues and eigenfunctions of a biharmonic operator on an arbitrary domain --$t22. Error estimates for eigenvalue problems --$tConclusion --$tBibliography 330 $aBack-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) and endangering the whole structure. By careful choices of geometry, materials and damping mechanisms, hazardous effects on wind engines, planes, turbines and cars can be avoided. Besides an introduction into the problem of flutter, new formulations of flutter problems are given as well as a treatise of supersonic flutter and of a whole range of mechanical effects. Numerical and analytical methods to study them are developed and applied to the analysis of new classes of flutter problems for plates and shallow shells of arbitrary plane form. Specific problems discussed in the book in the context of numerical simulations are supplemented by Fortran code examples (available on the website). 410 0$aDe Gruyter studies in mathematical physics ;$vVolume 25. 606 $aPlates (Engineering)$xVibration 606 $aShells (Engineering)$xVibration 606 $aElastic plates and shells$xMathematical models 615 0$aPlates (Engineering)$xVibration. 615 0$aShells (Engineering)$xVibration. 615 0$aElastic plates and shells$xMathematical models. 676 $a629.132/362 686 $aUF 4700$qSEPA$2rvk 700 $aAlgazin$b Sergei? D.$f1949-$01724814 702 $aKii?ko$b I. A$g(Igor' Anatol'evich), 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910809416003321 996 $aAeroelastic vibrations and stability of plates and shells$94127194 997 $aUNINA