1. Engineer/
Consultant
Onsite
Experience
 Heat Transfer Analysis on
Customer
 Notable projects on heat transfer problems:
Burst
Flight test measurement
Hands on experience in
verifying
Education
Bachelors in Aeronautical Engineering
Anna University, Chennai, India 2009
Projects handled
34 Rue Paul Decamps,
Toulouse-31300, France
+33 (0) 6 0567 87 24
dheenadhayalanaero@gmail.com
https://www.linkedin.com/in/
Deena-Aero
Tool Skills:
NX-IDEAS - Advanced
TMG (solver) - Advanced
PATRAN - Regular Use
ICEM CFD -Regular use
Programming Skills:
VBA Macros - Regular use
Shell scripting - Beginner
C - Begineer
Operating System:
Windows, UNIX
English :Fluent
Tamil :Native
French - Beginner
Field: Aerospace, Automotives
Job :
- Thermal Engineering – Heat
transfer Analysis on full aircraft
and structures like pylon, flap,
wing and avionic equipments.
- Heat Balance calculation – Hand
calculations.
- Mapping – Mapping the thermal
results on structural model
- Rapid decompression analysis
Experiences
AREAS OF INTEREST
LALANGUAGESEShttp://ww
DIGITAL COMPETENCES
Deenadhayalan SOMASUNDARAM
Aero-
Nationality
Availability
Objective:
myskills,experience, and education can be further developed and effectively used
CONTACT
Engineer/
Consultant
Altran Technologies India Pvt Ltd,
Bangalore
Onsite
Experience
Altran SUD OUEST, France
Heat Transfer Analysis on full aircraft and its structures (PYLON, APF and Flap
Customer: Airbus France/ Germany
The scope of this project is to perform transient hea
or local structures of the aircraft. The analysis is carried out by providing the heat and
sink source surrounding the structures with necessary (heat transfer m
condition such as conduction (Thermal contacts), convection (HTC), radiation (VF with
sky and ground) and CFD results to study the temperature reached
Following are the key responsibilities,
o Geometric and FE modelling of input geometry (aircraft structures) to make a fine
thermal model for analysis in IDEAS.
o Model validation and debugging the errors in boundary conditions
o Treatment of necessary boundary condition such as heat source (Engine data, CFD
data) and sink sources (wing fuel temperature).
o Performing the analysis and validating the results in accordance with customer
specification and needs.
Notable projects on heat transfer problems:
Burst and Fire Analysis:
o It is kind of catastrophic analysis performed on assumption of the sudden fire
burst inside pylon structures (bleed duct rupture or engine fire)
transfer and temperature reached on the structures.
o This task involves the preparing the model for fire
(BC’s were prepared with the convective and radiation value) and designing of fire
propagation.
Flight test measurement (FTI and FTR) vs Thermal model:
o This task involves, notifying the customer on interested structures for fixing the
thermocouples to retrieve flight test temperature measurements
o The measurements obtained from the flight test are compared with the thermal
model results (thermal model developed according to flight test environment) to
reason out the difference and make the modelling conservative for certification.
Hands on experience in projects like heat balance calculation
verifying the results) and mapping.
Education
Bachelors in Aeronautical Engineering- First class with distinction, CGPA (8.8/10)
Anna University, Chennai, India 2009
Projects handled
Experiences
Deenadhayalan SOMASUNDARAM, 25
-Thermal Engineer (Heat transfer Specialist
Nationality : Indian
Availability:2months notice period
Objective:Seeking a job in the domain of
myskills,experience, and education can be further developed and effectively used
Altran Technologies India Pvt Ltd,
2013 - Till date
March 2016 – till Date
structures (PYLON, APF and Flap)
Jan 2014–Till date
The scope of this project is to perform transient heat transfer analysis on aircraft model
. The analysis is carried out by providing the heat and
s with necessary (heat transfer modes) boundary
condition such as conduction (Thermal contacts), convection (HTC), radiation (VF with
to study the temperature reached over each structure.
Geometric and FE modelling of input geometry (aircraft structures) to make a fine
ugging the errors in boundary conditions
Treatment of necessary boundary condition such as heat source (Engine data, CFD
data) and sink sources (wing fuel temperature).
Performing the analysis and validating the results in accordance with customer
analysis performed on assumption of the sudden fire or
(bleed duct rupture or engine fire) to study the heat
structures.
This task involves the preparing the model for fire/burstscenario with suitable BC
BC’s were prepared with the convective and radiation value) and designing of fire
(FTI and FTR) vs Thermal model:
task involves, notifying the customer on interested structures for fixing the
thermocouples to retrieve flight test temperature measurements.
The measurements obtained from the flight test are compared with the thermal
model results (thermal model developed according to flight test environment) to
reason out the difference and make the modelling conservative for certification.
eat balance calculations (hand calculation for
First class with distinction, CGPA (8.8/10)
Anna University, Chennai, India 2009 – 2013
years
Heat transfer Specialist – 3 Years Experienced)
Seeking a job in the domain of thermal engineering where
myskills,experience, and education can be further developed and effectively used.