MARITA LOUIES D

adfujz@r.postjobfree.com

782-***-****

#*/*, * *** *****, pullaiyar koil Street, Ashok nagar, Bangalore- 560025

Objective

To work in an environment which encourages me to succeed and grow professionally where I can utilise my skills and knowledge appropriately.

Experience

Hindustan Aeronautics Limited

July 12th 2018 - August 19th 2018

Intern

During my training at HAL I was trained and exposed to various aircraft accessories and aircraft hangers of mirage, Hawk and Jaguar.

Umlaut Pvt Ltd

August 1st 2019 - December 31st 2019

Intern

Design and Analysis basics and software tools, such as Hypermesh, Optistruct Solver & Catia Meashing - 2D meshing, 3D meshing ( Tetra & Hexa), Linear Static Analysis, Modal Analysis. GD&T, F&DT

Aircraft basics and systems

Reading and analysing of engineering drawings

AxisCades

February 24th 2020 - Current

Graduate Trainee Engineer

Wing and landing gear repairs - perform FDT justification for design solutions on in- service damages.

Preparation of FDT Stress Assessment Sheets (FAS) and TAS. Knowledge of preparation of FDT Repair work file

Analyse and design modifications referring the Structural Repair Manual Calculation of Kt ( blend, spot- facing), blend depth and crack propagation.

Education

East West College of Engineering

2019

B.E

7.58

Mount Carmel PU College

2015

PUC

76

Sacred Heart Girls High School

2013

SSLC

81%

Skills

Hypermesh

Catia V5

Optistruct

Microsoft office

Solid edge

Projects

Aerodynamic Investigation on Extended Leading Edge Flap at Low Reynolds Number Eppler 423 airfoil was modified by placing a leading edge flap designed in CATIA V5 and analysed using

ansys. The results so obtained showed higher lift at low reynolds number, apt for use of lift generation for low

speed, heavy cargo airplanes.

Tools used – ansys (icem cfd, workbench) and catia v5 Fatigue Justification and Repair of wing and landing gear structure of in-service Aircrafts Propose appropriate repair solutions.

Preparation of FAS and TAS

knowledge of finding relevant check stress files for the application of weight variants ( of airbus family)

Preparation of F&DT Repair work file.

Knowledge in the application of SRM, AIRNAV ATA(51,52 ). TOOL USED:

Hand calculations on Fatigue and Crack propagation Airbus TechRequest

Airbus World- drawings, Aircraft MODs, SRM from airnavX Microsoft office

Language

English

Kannada

Hindi

Tamil

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