Depolymerizable bio-based multifunctional closed loop recyclable epoxy systems for energy efficient structures
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Construction Of Novel CERTification methOds and means of compliance for disruptive technologies
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Enabling Interlaminar Fracture Testing of MULTIdirectional composite LAMinates for safe and
efficient structures
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NOVEL LOW-PRESSURE CRYOGENIC LIQUID HYDROGEN STORAGE FOR AVIATION
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HYPERCONNECTED SIMULATION ECOSYSTEM SUPPORTING PROBABILISTIC DESIGN AND PREDICTIVE MANUFACTURING OF NEXT GENERATION AIRCRAFT STRUCTURES
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DEVELOPMENT OF A METHODOLOGY (TEST, MEASUREMENT, ANALYSIS) TO CHARACTERIZE THE BEHAVIOUR OF COMPOSITE STRUCTURES UNDER DYNAMIC LOADING
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THERMOPLASTIC MATERIAL ALLOWABLE GENERATION USING A RELIABILITY-BASED VIRTUAL MODELING PLATFORM
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OPTIMIZACIÓN DEL PROCESO DE DISEÑO COMPLETO DE LA ESTRUCTURA BORDE DE ATAQUE AERONÁUTICO
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MEJORA EN LA PRECISIÓN EN LA VALIDACIÓN Y VERIFICACIÓN DE ESTRUCTURAS
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IMPLEMENTATION CARBON FIBRES FOR ROTOR OF HIGH SPEED ROTATION MACHINE
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ROTATING COWLS FOR CLEANSKY, DESIGN AND MANUFACTURE OF A COMPOSITE ROTATING COWL
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DAMAGE TOLERANCE DESIGN FOR THIN PLY TEXTILE COMPOSITESTION MACHINE
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VIRTUAL TESTING AND STRUCTURAL MONITORING OF COMPOSITE STIFFENED PANELS CONSIDERING ENVIRONMENTAL EFFECTS
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HIBRIDACIÓN LOCAL DE MATERIALES COMPUESTOS LAMINADOS PARA MEJORAR SU TOLERANCIA AL DAÑO
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INTEGRATED METHOD FOR STRUCTURAL DESIGN OF COMPOSITE COMPONENTSNMENTAL EFFECTS
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DEMOSTRADOR DE UN “GRID” VIRTUAL DEVELOPMENT AND VALIDATION OF NON-CONVENTIONAL LAMINATES
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MORE AFFORDABLE AIRCRAFT THROUGH EXTENDED, INTEGRATED AND MATURE NUMERICAL SIZING
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MULTIFUNCTIONAL AND DAMAGE TOLERANT COMPOSITES: INTEGRATION OF ADVANCED CARBON NANOFILLERS AND NON-CONVENTIONAL LAMINATES
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CANFRANC UNDERGROUND PHYSICS
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DEMOSTRADOR DE UN “GRID” PARA ACTIVIDADES DE SIMULACIÓN CON REQUERIMIENTOS EXTREMOS DE CÁLCULO = “GRID” FOR SIMULATION ACTIVITIES FOR EXTREME CALCULATION REQUIREMENTS
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INVESTIGATION AND DEVELOPMENT OF INTELLIGENT AND SUSTAINABLE TECHNOLOGIES FOR COMPOSITE STRUCTURES
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DEVELOPMENT OF A METHODOLOGY TO ASSESS THE DAMAGE TOLERANCE TO FATIGUE LOADS OF BONDED JOINTS FOR COMPOSITE AIRCRAFT REPAIRS
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