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CV: Stress Engineer - Aerospace Research Engineer
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Date Submitted: Last Modified: Current job: Employment Term: Job location: Date available: Industry: KeywordsStress Engineer at Rücker Aerospace GmbH
Aerospace Research Engineer - collaboration with DLR and UNINA
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University Education |
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• Dates (from – to) • Title of qualification awarded |
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October 2008 – November 2011 Ph.D. in “Aerospace Engineering” |
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• Name and type of organisation providing education and training |
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University of Naples Federico II, Engineering faculty |
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• Final Marks |
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Excellent |
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• Dates (from – to) |
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August 29, 2011 – October 31, 2011 |
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• Name and type of organisation providing education and training |
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Visiting Ph. D. studentat the Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan, USA |
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• Dates (from – to) |
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October 2000 – May 22, 2008 |
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• Name and type of organisation providing education and training |
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University of Naples Federico II, Engineering faculty, Degree (BA+MA) in Aerospace Engineering |
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• Principal subjects / Occupational skills covered |
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Aerodynamics, Hypersonic Aerothermodynamics, Aircraft and Spacecraft Propulsion, Aircraft Design, Dynamics and Control of Spacecraft |
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• Final Marks |
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110/110 with honours (average mark exams: 29.8/30) |
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Remarkable Research Experiences |
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• Name and address of employer |
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German Aerospace Center(DLR), Germany University of Naples “Federico II”, Italy |
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• Dates (from – to) |
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January 2013 – Today |
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• Main activities and responsibilities |
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Study about the Aerodynamic behaviour of SpaceLiner 7.1 • Simulation with the particle code 3D-Direct simulation Monte Carlo and application of the Wilmoth Bridging formula. SpaceLiner, designed by DLR,is visionary, extremely fast passenger transportation concept, it should be able to fly the distance from Sydney to Western Europe, carrying 50 passengers. in no more than 90 minutes For more information about SpaceLiner an article appeared on Lufthansa magazine of February 2013 (pages 68-71): http://www.lhm-lounge.de/lh_1302_interkonti/lh_1302_inter_doppel.pdf |
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• Name and address of employer |
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Italian Aerospace Research Center (CIRA), Italy German Aerospace Center(DLR), Germany |
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Dates (from – to) |
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November 2010 – November 2012 |
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• Main activities and responsibilities |
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Study of DLR vehicle in low density regime Low-Density Effects on Suborbital Flight (DSMC Validation and Simulations)- FAST20XX project • Demonstration and validation of the numerical tools able to predict aero-thermal loads acting on a space re-entry vehicle at high altitude conditions. Characterization of the DLR low density wind tunnel V2G and aerodynamic analysis of the available model of a lifting body. • Study of the high altitude effects to the future hypersonic re-entry vehicle SpaceLiner 4. |
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Work Experience |
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• Name and address of employer |
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Rücker Aerospace GmbH –
HTP-Helikopter Technologie Park |
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• Dates (from – to) |
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March 1, 2013 – Today |
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• Main activities and responsibilities |
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Strength Static Validation for all structure parts of the A350-900XWB After Cargo Door (ACD), Bulk Cargo Door (BCD) and Forward Cargo Door (FCD), in collaboration with Korean Air Damage Tolerance Analysis, Plain Strength Analysis, Joint Strength Analysis, Buckling Analysis, Unfolding Analysis using MSC Patran/Nastran, HyperMesh, HyperView,Jet, Isami and creation of Excel macros |
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External training: “HyperMesh & HyperView”, by Altair, Böblingen – Germany,June 10-13 2013 |
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• Name and address of employer |
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Premium AEROTEC GmbH on behalf of GECI International Haunstetter Str. 225,86179 Augsburg |
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• Dates (from – to) |
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October 15, 2012 – February 22, 2013 |
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• Main activities and responsibilities |
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Request For Design Rework,using Excel sheets Side Shell Section 16-18 Bracket Stress Calculation, using MSC Patran/Nastran and Isami Tools, (Checker activity) ISAMI internal Trainingabout: Transverse Assembly (Composite Frame), Damage Tolerance Analysis, Filled Hole Analysis, Bolted Joint 1D Analysis, Panel Buckling Analysis, Open Hole Analysis, Tension Fitting, Static Lug Analysis, Metallic Panel Energetic Rayleigh Ritz Analysis, Plane Super Stiffener Sizing. November 5-9, 2012 |
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• Name and address of employer |
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GECI international GmbHHanna-Kunath-Strasse 4, 28199 Bremen |
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• Dates (from – to) |
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April 10, 2012 – October 12, 2012 |
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• Main activities and responsibilities |
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Hand calculation for A350 Pax Door surround unloaded brackets, A400M bracket impact on primary structure calculation, mechanical brackets stress report, using MSC Patran/Nastran and Excel sheets |
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External training: “CATIA V5 FOR STRESSMAN”, by EADS Learning Services, Hamburg – Germany,September 24-26 2012 |
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• Name and address of employer |
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Aerosoft S.p.ACentro Direzionale, 80143. Naples, Italy. |
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• Dates (from – to) |
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November 28, 2011 – March 30, 2012 |
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• Main activities and responsibilities |
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A350 XWB-MLGB: Static Analysis of some component for the Main Landing Gear Bay (Central Pressurized Floor and Bulkhead),: more specifically DFEM creation and simulation of External seat rail using MSC Patran/Nastran; Lug analysis for Z-strut and Y-strut using the Isami Tools. Piaggio P1XX: Stress Analysis on P1XX Central and Rear Fuselage Structure. Update of the complete 3D GFEM Model, using MSC Patran/Nastran |
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Personal skill and competences
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Mother Tongue |
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Italian |
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Other languages |
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English: advanced; German: beginner LANGUAGE COUSES: English: • Upper Intermediate, EF International Language Schools, Manchester, July 4, 2011 – August 12, 2011 • Advanced and Business, Wall Street Institute, Bremen/Munich, July 23, 2012 – January 23, 2013 German: • Beginner, inlingua Augsburg | Sprachschule und Sprachkurse Augsburg, April 30, 2013 – Today |
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Social skills and competences |
Strong will. Self-confidence. Flexibility and acceptance, work confidently within a group. Willing to learn fast and to embrace new challenges. Successfully adaptation to situations & environments changing. Determination to persevere through difficult situations. Available to travel
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Computer skills
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Engineering Software: MSC Nastran/Patran, ISAMI, HyperMesh & HyperView Catia V5, Matlab, Tecplot, Fluent, Gambit, Rhinoceros Programming Languages: C/C++, Fortran, able to create Excel Macros Operating Systems: DOS, Windows OS Microsoft Applications: Word, Excel, Power Point. |
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Further Information |
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Participation to |
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Couses: |
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• “Aircraft Structures Design and Analysis” byMichael Mohaghegh, Mark S. Ewing University of Kansas Aerospace Short Course, Orlando, Florida November 11-15, 2013 |
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• “Scructural Analysis MSC Nastran/Patran” byAlmatech Software, Centro direzionale, Napoli November 21-25, 2011 |
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• “General 3-D DSMC Codes with Emphasis on NASA’s DSMC Analysis Code (DAC)” by G. J. LeBeau, F. E. Lumpkin of NASA Johnson Space CenterSanta Fe, New Mexico, USA, September 25, 2011 |
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Congresses: |
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• “28th International Symposium on Rarefied Gas Dynamics”, Escuela de Ingenieros de la Universidad de Zaragoza, Spain, July 9-13, 2012
• “Direct Simulation Monte Carlo 2011: Theory, Methods, and Applications (DSMC11)”, Santa Fe, New Mexico, USA,September 26-29, 2011
• “27th International Symposium on Rarefied Gas Dynamics”, Asilomar Conference Grounds Pacific Grove, California, USA July 10-15, 2010 |
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Workshops: |
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• FAST20XX Final Presentation MeetingInstitute of Space Systems, (DLR), Bremen, Germany,November 27 - 29, 2012
• 3rd SpaceLiner Design Workshop Institute of Space Systems, (DLR), Bremen, Germany,August 2-3, 2012 |
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Journal Publications |
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L. Morsa, G. Zuppardi, R. Votta, A. Schettino Influence of Chemical Models on the Heat Flux for Expert and Orion capsules To appear on Journal of Aerospace Engineering, 2013
G.Zuppardi, L.Morsa Evaluation of non-equilibrium by the Crocco Theorem Journal of Aerospace Engineering, Vol.225 Part G, N.9, 2011, pp 985-994
G.Zuppardi, L.Morsa, F. Romano Influence of chemical models on the computation of thermo-dynamic parameters in hypersonic, rarefied flow Journal of Aerospace Engineering, Vol.224 Part G, N.6, 2010, pp 637-646 |
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Conference Publications |
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L. Morsa, G. Festa and G. Zuppardi Sensitivity Analysis of the Gupta and Park Chemical Models on the Heat Flux by DSMC and CFD Codes Proceedings of the 28th International Symposium on Rarefied Gas Dynamics (RGD28), Zaragozza (Spain), July 2012
R. Votta, M. Marini, L. Morsa, G. Fels, G. Zuppardi, T. Schwanekamp and M. Sippel Analysis of Low-Density Effects in Suborbital Flight of FAST20XX, Proceedings of the 28th International Symposium on Rarefied Gas Dynamics (RGD28), Zaragozza (Spain), July 2012
R. Votta, G. Ranuzzi, M. Marini, L. Morsa, G. Fels, T. Schlegat and K. Hannemann, Numerical and Experimental Analysis of Low-Density Effects in Suborbital Flight of FAST20XX, 43rd AIAA Thermophysics Conference, New Orleans, Louisiana (USA), AIAA-2012-3107, June 2012
G.Zuppardi, L.Morsa Effects of the Chemical Models by Park and by Gupta on Thermo-Fluid-Dynamic Parameters in Continuum Low Density Regime Direct Simulation Monte Carlo 2011: Theory, Methods, and Applications (DSMC11) September 2011. Santa Fe, New Mexico, USA,
L. Morsa, G. Zuppardi, A. Schettino, R. Votta Analysis of Local Bridging Formulae in Transitional Regime Proceedings of the 27th International Symposium on Rarefied Gas Dynamics (RGD27), Pacific Grove (USA), July 2010
G. Zuppardi, L. Morsa, A. Schettino, R. Votta Analysis of Aero-Thermodynamic Behaviour of EXPERT Capsule in Transitional Regime Proceedings of the 27th International Symposium on Rarefied Gas Dynamics (RGD27), Pacific Grove (USA), July 2010
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Publications in Preparation |
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L. Morsa and G. Zuppardi Influence of Ionization for the Gupta and the Park Chemical models to be presented at Proceedings of the 28th International Symposium on Rarefied Gas Dynamics (RGD29), Xi'an (China), July 2014
G. Zuppardi, L. Morsa , T. Schwanekampand M. Sippel Aero-Thermo-Dynamic Analysis of Spaceliner vehicle in High Altitude Flight to be presented at Proceedings of the 28th International Symposium on Rarefied Gas Dynamics (RGD29), Xi'an (China), July 2014
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