LEADER 00721cam0-22002771i-450- 001 990006699280403321 005 20070625112949.0 035 $a000669928 035 $aFED01000669928 035 $a(Aleph)000669928FED01 035 $a000669928 100 $a20010426d1969----km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $aSperanza e storia$fJosef Pieper 210 $aBrescia$cMorcelliana$d1969 215 $a120 p.$d22 cm 225 1 $a<>pellicano 700 1$aPieper,$bJosef$0160401 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990006699280403321 952 $aII A 26$b4252$fFSPBC 959 $aFSPBC 996 $aSperanza e storia$9616139 997 $aUNINA LEADER 02489nam 2200445 450 001 9910795472103321 005 20230803043537.0 010 $a3-8325-9334-9 035 $a(CKB)4340000000244336 035 $a(MiAaPQ)EBC5247085 035 $a(Au-PeEL)EBL5247085 035 $a(CaPaEBR)ebr11539814 035 $a(OCoLC)1021805567 035 $a58a1c693-9e40-499a-8417-3edeb0dd2d03 035 $a(EXLCZ)994340000000244336 100 $a20180521d2013 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAnalysis of process-induced distortions and residual stresses of composite structures /$fChristian Brauner 210 1$aBerlin :$cLogos,$d[2013] 210 4$dİ2013 215 $a1 online resource (x, 155 pages) $cillustrations 225 0 $aScience Report aus dem Faserinstitut Bremen ;$vBand 8 300 $aPublicationDate: 20131029 311 $a3-8325-3528-4 330 $aLong description: The increased application of composite materials in lightweight structures leads to new integral design of structural parts, using the example of, an integral composite landing flap of an Airbus A320 aircraft. This offers possibilities to simplify the process chain, to decrease manufacturing costs and to have fibre fair structural design. The critical disadvantage of large integral designs is that process-induced deformations are a risk factor during the design phase of the manufacturing process, because rework is not always possible. Especially, the aircraft industry with its demands on high qualities / tolerances and the application of hot curing resin systems, requires knowledge-based methods for virtual process design to avoid time- and effort-consuming iterations. This thesis contributes to the understanding of the mechanism behind process-induced distortions and stresses related to the Resin Transfer Moulding (RTM) manufacturing process. The aim is to comprehend the phenomena, to identify related parameters and to present compensation strategies. 606 $aDeformations (Mechanics) 615 0$aDeformations (Mechanics) 676 $a620.1123 700 $aBrauner$b Christian$01540934 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910795472103321 996 $aAnalysis of process-induced distortions and residual stresses of composite structures$93792843 997 $aUNINA