Abdelaziz Taib has over 15 years of experience as a stress engineer performing structural analysis of aircraft components. His experience includes working on projects for Aerolia Canada, Jetaviation, Bombardier, and École Polytechnique de Montréal. He has extensive knowledge of stress analysis techniques including hand calculations, finite element modeling, and fatigue and damage tolerance analysis.
Motivated Geologist with over thirteen years in Oil and Gas industry. Proficient in Well-site Geologist & Geo-Pressure Predict Engineer and Mud-Logging Data Engineer. Most experienced as one man Offshore Well-site Geologist in exploration well with high pressure and high temperature, and some horizontal production wells with very thin and critical target. Main clients worked with: Exxon Mobil, Shell, Talisman, Salamander, Premier Oil, Apache Energy, Idemitsu, Origin Energy, Petronas, KNOC
Good skills of persuading and communicating with different kind of people, especially when resolving problems and dealing with tight deadlines. Capable of working under the pressure as well as independently
Mechartes determined the behavior of critical temperature which results in longitudinal expansion of the pipeline, which might cause upheaval buckling and failure.
Computational Aerodynamic Prediction for Integration of an Advanced Reconnais...IJERA Editor
In this paper a computational aerodynamic prediction to support the aeromechanical integration of an advanced reconnaissance pod on a 5th generation fighter type aircraft is presented. The aim of the activity was to compare the aerodynamic characteristics of the new pod to a previous one already cleared on the same aircraft fleet, given verified inertial and structural similarity. Verifying the aforementioned aerodynamic similarity without involving extensive flight test activity was a must, to save time and to reduce costs. A two steps approach was required by the Certification Authority to verify, initially, the performance data compatibility in terms of aerodynamic coefficients of the old pod with the new one, in order to allow performance flight manual data interchangeability (a quantitative comparison was required); afterwards, a qualitative assessment was conducted to verify the absence of unsteadiness induced by the introduction in the external structure of the new pod of an auxiliary antenna case. Computational results are presented both for Straight and Level Un-accelerated Flight and Steady-Sideslip flight conditions at different Angles of Attack.
Dedicated Materials engineer and actually balanced between Integrity and Corrosion engineer, NACE member and holding NACE corrosion technician certificate and having solid experience in oil and gas field.
Topology optimization to guide the architecture of a BIW structure, challenge...Altair
For automotive industry, lightweight design is one of the five key factors among engine enhancement, aerodynamics, rolling resistance and energy management to overcome challenges due to environmental regulations. Thanks to new developments, recent models weigh 140 kg to 200 kg lighter than their predecessors. But to achieve more ambitious objectives in vehicle weight, structural design optimization is necessary at all stages of the design process. This presentation shows how topology optimization could be used very early to guide the body-in-white design and reach the best compromises between the vehicle performance expectations and the architecture constraints. We first remind how applying topology optimization for sheet metal design remains difficult. Then we explain the conditions for a success. The complete optimization process is detailed from the computation model building phase to the optimization results and their complex conversion into a design made from stamped or folded parts. Finally we conclude with a short summary about the topology optimization method and highlight some remained issues.
Speakers
Benoît Guillaume, Optimization expert, PSA Peugeot Citroën - Centre Technique de Vélizy A
Monitoring and Maintanance of On-shore pipeline ,Off shore pipeline ,Well jacket structure ,Jetty,Platform and storage tanks for the client of BRUNEI SHELL PETROLEUM
Motivated Geologist with over thirteen years in Oil and Gas industry. Proficient in Well-site Geologist & Geo-Pressure Predict Engineer and Mud-Logging Data Engineer. Most experienced as one man Offshore Well-site Geologist in exploration well with high pressure and high temperature, and some horizontal production wells with very thin and critical target. Main clients worked with: Exxon Mobil, Shell, Talisman, Salamander, Premier Oil, Apache Energy, Idemitsu, Origin Energy, Petronas, KNOC
Good skills of persuading and communicating with different kind of people, especially when resolving problems and dealing with tight deadlines. Capable of working under the pressure as well as independently
Mechartes determined the behavior of critical temperature which results in longitudinal expansion of the pipeline, which might cause upheaval buckling and failure.
Computational Aerodynamic Prediction for Integration of an Advanced Reconnais...IJERA Editor
In this paper a computational aerodynamic prediction to support the aeromechanical integration of an advanced reconnaissance pod on a 5th generation fighter type aircraft is presented. The aim of the activity was to compare the aerodynamic characteristics of the new pod to a previous one already cleared on the same aircraft fleet, given verified inertial and structural similarity. Verifying the aforementioned aerodynamic similarity without involving extensive flight test activity was a must, to save time and to reduce costs. A two steps approach was required by the Certification Authority to verify, initially, the performance data compatibility in terms of aerodynamic coefficients of the old pod with the new one, in order to allow performance flight manual data interchangeability (a quantitative comparison was required); afterwards, a qualitative assessment was conducted to verify the absence of unsteadiness induced by the introduction in the external structure of the new pod of an auxiliary antenna case. Computational results are presented both for Straight and Level Un-accelerated Flight and Steady-Sideslip flight conditions at different Angles of Attack.
Dedicated Materials engineer and actually balanced between Integrity and Corrosion engineer, NACE member and holding NACE corrosion technician certificate and having solid experience in oil and gas field.
Topology optimization to guide the architecture of a BIW structure, challenge...Altair
For automotive industry, lightweight design is one of the five key factors among engine enhancement, aerodynamics, rolling resistance and energy management to overcome challenges due to environmental regulations. Thanks to new developments, recent models weigh 140 kg to 200 kg lighter than their predecessors. But to achieve more ambitious objectives in vehicle weight, structural design optimization is necessary at all stages of the design process. This presentation shows how topology optimization could be used very early to guide the body-in-white design and reach the best compromises between the vehicle performance expectations and the architecture constraints. We first remind how applying topology optimization for sheet metal design remains difficult. Then we explain the conditions for a success. The complete optimization process is detailed from the computation model building phase to the optimization results and their complex conversion into a design made from stamped or folded parts. Finally we conclude with a short summary about the topology optimization method and highlight some remained issues.
Speakers
Benoît Guillaume, Optimization expert, PSA Peugeot Citroën - Centre Technique de Vélizy A
Monitoring and Maintanance of On-shore pipeline ,Off shore pipeline ,Well jacket structure ,Jetty,Platform and storage tanks for the client of BRUNEI SHELL PETROLEUM
1. Abdelaziz TAIB
Canadian Citizen
644 Chemin Bord de l’Eau, 1
Laval, H7X 2W9, Canada
438 933 1701
abdelaziztaib.stress@yahoo.fr
Objective:
To obtain a challenging position in the field of Aircraft Structural Engineering where my training
and experience in development and design will be asset.
Professional Experience
• Stress Engineer (Aerolia Canada, Consultant) 02/2012 to 12/2014
- Stress Analysis (Composite and Metallic) of various Fuselage components for
Global 7000/8000 Program (Bellyfairing, Keel Beam, Emergency Door, Sills,
Root Frames and Intercostals).
- System Brackets.
- Weight saving proposals and presentations.
- Detailed analysis using traditional Airbus methodology - FEM load extraction.
- Generation of Stress Reports.
• Stress Engineer (Jetaviation, Basel, Switzerland ) 03/2009 to 07/2011
- Stress analysis of monuments (installations and assemblies) for custom interior
completion of Airbus 340/300 and 340/600.
- Stress analysis of floor structure and upper attachments for Airbus 340.
- Drafting of design compliance and stress reports for aircraft interior certifications.
• Stress Engineer-MRB (Bombardier, Canadair, Canada) 03/2008 to 03/2009
- Substantiation of repair designs of primary and secondary aircraft structures,
including fuselage, cockpit and empennage (Static & Fatigue Analysis).
- Investigation of urgent technical problems (e.g. manufacturing or production
defects) and recommendation of corrective action in a timely manner.
- Stress Analysis of various Cockpit components (Stringers, Frames, Joints and
Bulkhead).
- Damage Tolerance Analysis
- Generation and checking of Stress Reports.
• Stress Engineer (Bombardier, Completion, Montréal, Canada) 01/2006 to 02/2008
- Analysis of monuments (installations and assemblies) for Global XRS interiors.
- Drafting of design compliance and stress reports for aircraft interior certifications.
- Support for primary structure and interior modification design of the Global XRS.
- Standardization of Finite Element Modeling by developing a new methodology:
a- Cabinet Assembly in Catia V5 is transformed in Mid Surfaces and Point
Attachments accurately and finally exported to Patran.
b- FEM Model is created in Patran accurately and quickly.
c- Stress report is standardized by using Patran Post processor and Visual Basic.
2. • Research Associate at Centre de Recherche Appliquée sur les Polymères, CRASP
(Project from Seawind Aircraft Company, Quebec, Canada) 04/2004 to 05/2005
- Stress analysis of glass-fiber-reinforced vinylester composite laminates (Hand
Calculation and FEM using ANSYS).
- Collaborated with the CRASP team in the characterization and certification process
of new low-cost Seawind aircraft composite material according to Transport Canada
and FAA recommendations.
- Carried out experimental studies of the mechanical behaviour of bonded composite
joints for Seawind Company.
• Independent Business Owner/Operator (Algeria) 06/1996 to 12/2001
Tasks:
- Management and training of employees
- Sales and Repair of Automobile tires
- Balance and alignment of wheels
Skills
• Good knowledge in Fatigue & Damage Tolerance.
• Hand Calculation (Bruhn, Niu, Roark’s, Flabel, ESDU and Bombardier Strength Manual).
• Femap 10 (strong), Nastran/Patran 2010 (strong), Ansys 9.1, Catia V5 (strong), Enovia,
Smarteam, Autocad 2009, Solidworks 2004, Nasgro 6.2, Golhiat, Afgrow 4.1.
• Planetes V5 (CERCA Software for analysis of fluid based engineering systems).
• C, Fortran, VBA, MS Office, Mathcad 14.
Education
• Member of Ordre des Ingénieurs du Québec 06/2005 to 12/2005
Courses taken:
- Advanced Strength Of Materials
- Mechanical Design of Machine Elements
- Fatigue and Damage Tolerance
• Master of Science, Aerospace Engineering 01/2002 to 04/2004
Major: Aircraft Composite Material
École Polytechnique de Montréal
• Bachelor of Degree, Mechanical Engineering 09/1990 to 07/1995
Major: Mechanical Engineering
Blida University (Algeria)
3. Technical projects
• École Polytechnique de Montréal 01/2003 to 06/2004
- Master’s Project
Nonlinear Finite Element and Experimental Analysis of Composite Adhesive
Bonded Joints.
- Case study with Pratt & Whitney Canada
Parametric study of the thermodynamic cycle of a turbopropeller: technological
limits, off-design, transient state and stability. Stress analysis of turbine blade and
turbine blade attachment.
- Numerical study of incompressible flow (Fortran, Planetes V5)
Method based on the solution of Navier-Stokes equations using the finite volume
method.
- Study of compressible flow (language C)
Analytic and implicit finite difference method.
• University of Blida 09/1994 to 07/1995
- Research Project
Elaboration of a numerical software for the study of heat transfer in transient
regime, applied on simple geometries (wall, semi-infinite wall, cylinder and
sphere), by the use of the finite difference method and comparison with analytical
methods.
Publications
Abdelaziz A. Taib, Rachid Boukhili, Saïd Achiou, Sébastien Gordon and Hychem
Boukehili, "Bonded Joints with composite adherends. Part I: Effect of specimen
configuration, adhesive thickness, spew fillet and adherend stiffness on fracture".
International Journal of Adhesion and Adhesives Volume 26, Issue 4, July 2006, Pages
226-236
Abdelaziz A. Taib, Rachid Boukhili, Saïd Achiou and Hychem Boukehili "Bonded
Joints with composite adherends. Part II: Finite element analysis of joggle lap joints".
International Journal of Adhesion and Adhesives Volume 26, Issue 4, July 2006,
Pages 237-248
Languages
English, French, Arabic, Berber.
Activities
• Soccer, chess, cycling, judo.
• Reading, traveling.