Thierry GALLOIS
Born April, 30th 1975
Fluid
Dynamics Engineer
MEng MSc PhD
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Scope of Intervention
Field
of competences in fluid dynamics, aerodynamics, hydrodynamics and
energetics,
Numerical
simulation, CFD code development
Management
and design of tests and experimental validations in fluid dynamics,
Management
of R&D projects and team, design office…
Education
2004
Advances
in aeroacoustics
Von
Karman Institute for fluid dynamics Lecture Series, Belgium.
1999-2003 Ph.D.,
fluid mechanics
University
of Orleans, France.
1998-1999 M.Sc.,
aerodynamics
University
of Orleans, France.
Aerodynamics,
fluid dynamics, compressible flow,
multiphasic flow,
thermodynamics... Computational fluid dynamics, experimental methods
in fluid: LDA, PIV...
1996-1999 M.Eng.,
energetics & fluid dynamics
ESEM
(Engineer superior school for materials and energetics), Orleans,
France.
Fluid
dynamics, Energetics, thermics,
combustion,
thermodynamics, Computer Science, Materials, CAD...
Professional
Experiences
Since Feb 2006:
Aerodynamic Systems Manager NSC
Group (260 employees, T.O. 160M€) : World Leader for Non-woven
textile machinery
- in progress... - Head of
all air related subjects of a textile machinery manufacturer group
R&D Projects
manager
- Aerodynamic optimisation of air
transferred non-woven web devices : new design,
validations and -30% cost achievement.
- New fans design and
validation
- Aerodynamic barrier of high speed non-woven
web production investigation : +40% production achieved, new devices to
be proposed to customers
- Mechanical and
textile efficiency : prototypes designed and validated, now in
production in UK, USA, Turkey, Spain…
- Aerodynamic optimisation of air
transferred non-woven web devices : new design,
validations and -30% cost achievement.
- Survey of textile
machinery parameters of production with aerodynamic tools : patented
Design Office
- Air handling systems design and calculation
- Cost killing of existing devices
- Management in design office : technicians
and projects
After Sale
- Failure investigation
- Setup and fine tuning of air systems during
warranty period
2005:
Mechanical
Engineer CILAS (200
employees, T.O. 25M€), EADS group.
-
2 months - MegaJoule Laser project.
- In charge of optical
amplifier definition proofreading procedure (reports, contractual
documentation) for CEA review of definition.
- Evaluation of particularities required by
customer (CEA),
- Managing the conformity of the definition
towards schedule of conditions,
- Preparation of tests for
conformity validation.
2003-2004 : Aerodynamics
Engineer LME (Laboratory
for Mechanics and Energetics), Orleans,
France
-
18 months - In charge of numerical studies and experimental
validations in aerodynamics within industrial matters.
Low Reynolds number
lifting surfaces
- Team : with 1 undergraduate student,
- Objectives : Experimentally settle
results from high Reynolds number flows to low Reynolds number flows in
terms of vortices and over lift phenomena,
- Achievement : 3D unsteady Fluent
simulation,
Experimental design for wind tunnel testing,
Experimental planning and results analysis,
- Tools : Fluent, Wind tunnel,
pressure probes, 1D aerodynamic balance.
Aeromechanical behaviour of a lightweight UAV (Bertin
Technology)
- Team : with 1 assistant eng., 2
technicians (electronics & mechanics),
- Objectives : Experimental
investigation of flight domain over 1200 flight configurations (sweep,
incidence, oncoming flow velocity, rpm...),
- Achievement : Totally new wind
tunnel mounting system,
Configuration of 6D aerodynamic balance,
Configuration of analogue data acquisition device ,
Experimental planning and results analysis,
- Tools : Fluent, Wind tunnel,
pressure and velocity probes, 6D aerodynamic balance.
Optimisation of endurance race cars aerofoil (PSA
customer team)
- Team : with 1 PhD graduated eng., 1
assistant eng., 4 undergraduate students,
- Objectives : In order to reduce top
speeds, FIA rules stand for smaller span aerofoil. The purpose of the
study was to reach aerodynamic performance when airfoil span is reduced,
- Achievement : 2D airfoil numerical
investigation,
3D numerical investigation (distributed Fluent calculus with 2 –
3 millions cells),
Experimental validations,
Solutions reduced to two major aerofoil configurations,
- Tools : Xfoil, Fluent, Wind tunnel,
pressure and velocity probes, 6D aerodynamic balance.
Air conditioning
circuits design for regional transport aircraft (Daher)
- Team : with 1 PhD student,
- Objectives : Air conditioning in
transport aircraft uses highly winding circuits. Head losses in
particular junction have been numerically investigated and compared
with experimental results,
- Achievement : 3D Fluent
investigation,
Good Accordance with experimental measurement of head losses,
- Tools : Fluent.
2002-2004 : Fluid
dynamics and Computer Science Lecturer
-
24 months - Full time temporary position in Polytechnic School of
University of Orleans
- Lecturer and developer of
the Fluid dynamics and Computer Science courses.
- Theoretical and numerical fluid dynamics
(Fluent, Gambit, Digital Wind tunnel),
- Tutorials in fluid dynamics (testbeds and
wind tunnels),
- Aerotechnics,
- Computer science and numerical mathematics,
- Industrial tutorials:
- Helicopter rotor wake simulation (with ONERA
financial support – 40k€),
- Development of a simulation tool for rotor
wake interaction in helicopters and wind turbines,
- Lightweight aircraft design (with Wichita
State University),
- Head of mini UAV (unmanned aerial vehicle)
design team at Orleans University: ONERA (French aeronautics and space
research centre) and DGA (the French Arms Procurement Agency, of the
Ministry of Defence) organized an International Universities mini UAV
competition, opened to engineering schools and universities.
- Team with two Lecturers and 16
students from 2 Engineering schools.
- 2003: Team awarded grant money (40 k€)
for the technical feasibility and operational interest presented in the
definition report.
- 2004: prototype of the vehicle
without optical nor laser sensors.
1999-2002 : Fluid
dynamics Research Engineer
-
36 months - Full time temporary position at CNRS, Orleans, for PhD
preparation.
- After having reviewed main works
about lifting-line and numerical treatment of Hadamard's sens finite
part integrals, we expose an implicit formulation of a steady lifting
line for curved and swept wings. We first compare our results with
Prandtl's lifting line theory and then validate them with a lifting
surface method. We show good accordance in terms of vorticity even with
highly curved wings.
- An application is shown in a
configuration closed to helicopter
rotor to show feasibility of our approach to this critical case.
- We propose an implicit method for unsteady
curved and swept lifting line time-marching numerical computation. A
numerical implementation is drawn in the most critical case of the
instantaneous gust entry. The results, even for highly curved wings,
are consistent relative to time discretization with good accordance
with unsteady high level lifting surface methods.
- 2 Publications in international Journals
(Computational Mechanics, 2002, 2006).
- 1 presentation during international
conference (2005).
- 3 presentations during national conferences
(2001, 2003, 2005).
- 2 research contracts with ONERA (15 k€
& 60 k€).
- Computational Fluid
Dynamics instructor
- ENSICA (Engineering school in
the aerospace fields), Toulouse.
- ESEM (Engineering school in the
materials and energetics fields), Orleans.
Technical
and Linguistic Skills
- English: fluent.
- French mother tongue.
- Russian: spoken, read.
- MS Windows &
Office (all versions), Linux (Mandriva), OpenOffice.
- Fortran (77/90), C,
LaTeX.
- Calculation software: Fluent, Gambit,
Digital Wind Tunnel...
- Data analysis and acquisition software:
Techplot, SigmaPlot, MatLab, Labview...
- CAD: SolidWorks.
- Computer science: hardware & software.
Futher Information
- French nationality.
- Married, one son (18 months).
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