Schwarzer Rumpf Realisierung von CFK Rumpfkomponenten unter Einbeziehung des Concurrent Engineering : Schlussbericht ; HGF Verbundprojekt: 99 19 ; Laufzeit: 01.07.1999 30.06.2002 Composite CFRP aircraft construction fuselage concurrent engineering impact and residual strength 3D thermal analysis 3D stress analysis buckling post buckling fire safety crash worthiness high velocity impact manufacturing technology joining technology design concepts manufacturing costs