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101 0 $aita
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200 1 $aStresses in shells$fBy Wilhelm Flugge.
210   $aBerlin$cSpringer-Verlag$d1960
215   $aXI, [1], 499 p. ill. 24 cm
610 0 $aCostruzioni aeronautiche
700  1$aFlugge,$bWilhelm
801  0$aIT$bUNINA$gRICA$2UNIMARC
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