Product development responsible, assessing best design solutions according to costs, deadlines, product safety, normative, CFD compliance with experimental tests and structural integrity at each stage of product maturity.Structural and CFD engineer specialist prior to start-up conception (June 2016, part time)

Focal point between Altran MRB engineering Team (Spain) and customer (Airbus A220) in FAL.

Ingeniero de Liaison (MRB firma delegada) proporcionando disposiciones para todo tipo de no conformidades durante el ensamblaje y preflight en FAL del programa A220 (anterior CSeries), asegurando que la certificación, seguridad, integridad y calidad del producto no quedan afectados, satisfaciendo las especificaciones del cliente.

MRB Liason engineer giving support to production by providing repairs and production line stopper design changes on discrepant items during construction, assembly and testing in FAL of any A220 (former Bombardier CSeries) aircraft ensuring that the basis of certification, safety, integrity and quality of the product are not adversely affected and that the aircraft is safe, durable and pleasing to the customer.

A380 S19Results comparison and sensitivity analyses between CASA Legacy Tools and equivalent ISAMI and ISAMI Xpress modules for the coming Legacy Tools to ISAMI migration.Stress analyses of some A380 S19 metallic and composite frames to composite skin joints. Verification checks and validation documents of A380 S19 GFEM and DFEMs employed in the strength calculation of joints.

A330 NEO HTP, A380 Main Landing Gear Doors & S19Stress Engineer giving support to MRB department. Analyses and static justifications in order to asses design solutions for manufacturing and assembly deviations against the aircraft design requirements. Compilation of non-conformities and concession reports (JMD, SCR) as well as disposition of remedial actions required. Consulting of HNCs through SAP.Damage tolerance, Buckling and Joint analyses of composite primary structure… Show more A330 NEO HTP, A380 Main Landing Gear Doors & S19Stress Engineer giving support to MRB department. Analyses and static justifications in order to asses design solutions for manufacturing and assembly deviations against the aircraft design requirements. Compilation of non-conformities and concession reports (JMD, SCR) as well as disposition of remedial actions required. Consulting of HNCs through SAP.Damage tolerance, Buckling and Joint analyses of composite primary structure through several stress tools such as ISAMI (FH, CBA, PSP, R2C, BJ2D, SSP), CASA Legacy Tools (URCO, COFUS, ANCOLAB), Nastran, Patran, VBA, Excel. Show less

A350-1000 Wing Lower Cover, estructura primariaEfficient modification, analyses and post-processing of complex DFEM models to perform Damage Tolerance, Buckling and Bolted Joints analyses of an advanced composite structure through the employment of several stress tools: ISAMI, Nastran, Patran, HyperMesh, Excel, VBA.Compilation of Strength Justification Reports.

Clean Sky project, BLADE programmeNew Airbus A340-300 Hybrid Wing Box Structure using advanced materials to achieve aerodynamic drag reduction by a laminar wing design.Linear Static Sizing, Strength Justification and Buckling analyses of different Wing Lower Cover structural components such as Skin, Stringers, Bolted Joints and Interfaces through the generation, analysis and post-processing of FEM models and the use of a broad range of standard hand and computer stress tools… Show more Clean Sky project, BLADE programmeNew Airbus A340-300 Hybrid Wing Box Structure using advanced materials to achieve aerodynamic drag reduction by a laminar wing design.Linear Static Sizing, Strength Justification and Buckling analyses of different Wing Lower Cover structural components such as Skin, Stringers, Bolted Joints and Interfaces through the generation, analysis and post-processing of FEM models and the use of a broad range of standard hand and computer stress tools. Compilation of Strength Justification Reports.Airbus UK Legacy Tools (APAs, ABSs, AJF), ESDU, Nastran, Patran, Excel, VBA, Abaqus, Catia Show less

Stress Engineer of secondary structure. A350 HTPF&DT Engineer of primary structure. A380 S-19Strength and Fatigue and Damage Tolerance analyses of composite and metallic components of primary and secondary structureISAMI, Nastran, Patran, Excel

R&D Internship in Aernnova EngineeringMEng final project workAerodynamic analyses of different airfoils and wings using a CFD program and further comparison with classic theories and empirical results.Final project work “Aerodynamic design of Booster wing and/or empennage” gained with honoursOpenFoam, AVL (Vortex-lattice method), ESDU, NACA Data Base, Catia