CV: Stress Engineer - Aerospace Research Engineer


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Candidate Profile
 Date Submitted:07-09-2013
 Last Modified:08-09-2013 (02:23)
Job information
 Current job:Stress Engineer - Aerospace Research Engineer
 Employment Term:Permanent
 Job location:Anywhere
 Date available:within a month
 Industry:Consulting/Engineering Services, Space Tourism
 KeywordsHypersonic Aerothermodynamics: Aero-Thermodynamic study of Space vehicles using DSMC codes, FLUENT * Aerospace Structure: DFEM - GFEM creation, Strength Static Validation using Patran/Nastran, HyperMesh, HyperView, Jet, Isami and Excel macros creation
CV

Stress Engineer at Rücker Aerospace GmbH

Aerospace Research Engineer - collaboration with DLR and UNINA

University  Education

• Dates (from – to)

Title of qualification awarded

 

October 2008 – November 2011

Ph.D. in  “Aerospace Engineering

• Name and type of organisation providing education and training

 

University of Naples Federico II,

Engineering faculty

 

• Final Marks

 

Excellent

 

• Dates (from – to)

 

August 29, 2011 – October 31, 2011

 

 

     

• Name and type of organisation providing education and training

 

Visiting Ph. D. studentat the Department of Aerospace Engineering,

University of Michigan, Ann Arbor, Michigan, USA

 

• Dates (from – to)

 

October 2000 –  May 22, 2008

 

• Name and type of organisation providing education and training

 

University of Naples Federico II, Engineering faculty, Degree (BA+MA) in Aerospace Engineering

 

• Principal subjects / Occupational skills covered

 

Aerodynamics, Hypersonic Aerothermodynamics, Aircraft and Spacecraft Propulsion, Aircraft Design, Dynamics and Control of Spacecraft

 

• Final Marks

 

110/110 with honours (average mark exams: 29.8/30)

 

 

Remarkable Research

Experiences

 

 

 

• Name and address of employer

 

German Aerospace Center(DLR), Germany

University of Naples “Federico II”, Italy

    

• Dates (from – to)

 

January 2013 – Today

 

• Main activities and responsibilities

 

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

 

     

• Name and address of employer

 

Italian Aerospace Research Center (CIRA), Italy

German Aerospace Center(DLR), Germany

  

Dates (from – to)

 

November 2010 – November 2012

 

• Main activities and responsibilities

 

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.

 

Work Experience

 

 

 

• Name and address of employer

 

Rücker Aerospace GmbH –

HTP-Helikopter Technologie Park
Dr Ludwig BölkowStraße 1D-86609 Donauwörth

 

• Dates (from – to)

 

March 1, 2013 – Today

 

• Main activities and responsibilities

 

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

 

 

External training: “HyperMesh & HyperView”,

by Altair,

Böblingen – Germany,June 10-13 2013

 

 

• Name and address of employer

 

Premium AEROTEC GmbH

on behalf of GECI International

Haunstetter Str. 225,86179 Augsburg

 

 

• Dates (from – to)

 

October 15, 2012 – February 22, 2013

 

• Main activities and responsibilities

 

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

 

• Name and address of employer

 

GECI international GmbH

Hanna-Kunath-Strasse 4, 28199 Bremen

 

• Dates (from – to)

 

April 10, 2012 – October 12, 2012

 

• Main activities and responsibilities

 

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  

 

 

External training: “CATIA V5 FOR STRESSMAN”,

by EADS Learning Services,

Hamburg – Germany,September 24-26 2012

 

 

• Name and address of employer

 

Aerosoft S.p.A

Centro Direzionale, 80143. Naples, Italy.

 

• Dates (from – to)

 

November 28, 2011 – March 30, 2012

 

• Main activities and responsibilities

 

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

 

Personal skill and competences

 

 

 

Mother Tongue

 

Italian

 

 

 

Other languages

 

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

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   

 

Computer skills

 

 

 

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.

Further  Information

 

Participation to

 

 

 

         

 

Couses:

 

 

 

 

 

 

•    “Aircraft Structures Design and Analysis” byMichael Mohaghegh, Mark S. Ewing

University of Kansas Aerospace Short Course, Orlando, Florida November 11-15, 2013

 

   

 

 

•    “Scructural Analysis MSC Nastran/Patran” byAlmatech Software, Centro direzionale, Napoli November 21-25, 2011

 

   

 

 

•    “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

 

       

 

Congresses:   

 

 

 

 

 

 

•     “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

 

 

 

 

 

 

 

 

 

Workshops:

 

 

 

 

 

•      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

 

 

 

 

 

 

Journal

Publications

 

 

 

 

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

 

 

Conference 

Publications

 

 

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

 

Publications in

Preparation

 

 

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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