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alessanacunaguardia
2025-10-16 22:52:59 +02:00
parent c3aa5d1e4f
commit ecbc135ea2
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@@ -1009,9 +1009,9 @@
'exp.airbus.title':'AIRBUS - Structural Design & Analysis Engineer',
'exp.airbus.where':'Madrid, ES',
'exp.airbus.p1':'Sviluppo e valutazione di <strong>riparazioni</strong> per componenti in composito e metallo.',
'exp.airbus.p2':'Progettazione parti per <strong>A350 HTP</strong> e <strong>Sezione 19</strong> (fusoliera posteriore) in <strong>CATIA V5</strong>.',
'exp.airbus.p2':'Progettazione parti per <strong>A350 HTP</strong> e <strong>Sezione 19</strong> (fusoliera posteriore) con <strong>CATIA V5</strong>.',
'exp.airbus.p3':'Interfaccia Design Office in produzione, garantendo integrità strutturale e compliance.',
'exp.airbus.p4':'Sviluppo di <strong>modelli numerici</strong> e simulazioni esplicite su meccanismi di danno nei compositi.',
'exp.airbus.p4':'Sviluppo di <strong>modelli numerici</strong> e simulazioni esplicite su meccanismi di danno nei compositi con Abaqus.',
'exp.dlr.title':'DLR - Tesi di Laurea · R&D Engineer',
'exp.dlr.where':'Stoccarda, DE',
@@ -1201,7 +1201,7 @@
'exp.airbus.p1':'Development and assessment of <strong>repair solutions</strong> for composite and metallic components.',
'exp.airbus.p2':'Part design for <strong>A350 HTP</strong> and <strong>Section 19</strong> (rear fuselage) in <strong>CATIA V5</strong>.',
'exp.airbus.p3':'Design Office interface in production, ensuring structural integrity and compliance.',
'exp.airbus.p4':'Development of <strong>numerical models</strong> and explicit simulations for composite damage mechanisms.',
'exp.airbus.p4':'Development of <strong>numerical models</strong> and explicit simulations for composite damage mechanisms in Abaqus.',
'exp.dlr.title':'DLR - Master Thesis · R&amp;D Engineer',
'exp.dlr.where':'Stuttgart, DE',
@@ -1389,7 +1389,7 @@
'exp.airbus.p1':'Entwicklung und Bewertung von <strong>Reparatur­lösungen</strong> für Verbund- und Metallbauteile.',
'exp.airbus.p2':'Teilekonstruktion für <strong>A350 HTP</strong> und <strong>Sektion 19</strong> (Heckrumpf) in <strong>CATIA V5</strong>.',
'exp.airbus.p3':'Schnittstelle Design Office in der Produktion; Sicherstellung von Strukturintegrität und Compliance.',
'exp.airbus.p4':'Entwicklung von <strong>numerischen Modellen</strong> und expliziten Simulationen zu Schadensmechanismen in Verbundwerkstoffen.',
'exp.airbus.p4':'Entwicklung von <strong>numerischen Modellen</strong> und expliziten Simulationen zu Schadensmechanismen in Verbundwerkstoffen in Abaqus.',
'exp.dlr.title':'DLR - Masterarbeit · R&amp;D Engineer',
'exp.dlr.where':'Stuttgart, DE',
@@ -1576,7 +1576,7 @@
'exp.airbus.p1':'Desarrollo y evaluación de <strong>reparaciones</strong> para componentes compuestos y metálicos.',
'exp.airbus.p2':'Diseño de piezas para <strong>A350 HTP</strong> y <strong>Sección 19</strong> (fuselaje trasero) en <strong>CATIA V5</strong>.',
'exp.airbus.p3':'Interfaz con Design Office en producción, garantizando integridad estructural y cumplimiento.',
'exp.airbus.p4':'Desarrollo de <strong>modelos numéricos</strong> y simulaciones explícitas de daño en compuestos.',
'exp.airbus.p4':'Desarrollo de <strong>modelos numéricos</strong> y simulaciones explícitas de daño en compuestos in Abaqus.',
'exp.dlr.title':'DLR - Tesis de Máster · R&amp;D Engineer',
'exp.dlr.where':'Stuttgart, DE',