*. PERSONAL DETAILS

*. EDUCATIONAL QUALIFICATIONS

# Degree

Name of the Institution/

Grade or % of Marks secured

%CGPA

1

BE

(Aeronautical Engineering) Aeronautical Society of India 60.5 2

MTech

(Aerospace Engineering)

Indian Institute of Technology,

Chennai 8.2

3 12th Board of Education, Haryana 74.5

4 10th Board of Education, Haryana 75.5

Publication

Conference paper in ICPMT July 2019, “Failure Analysis of Nose Landing Gear”. 3. PROFESSIONAL EXPERIENCE

Profile

Summary

Overall 3.9 years of experience

• Good experience in to Finite Element Modelling and Analysis by using tools ANSYS workbench, APDL, ABAQUS, HYPERMESH, HYPERVIEW and NASTRAN/PATRAN.

• Has experience in carrying out Linear, non-Linear and Modal analysis.

• Good experience in hand calculations.

• Also has good exposure in APDL.

• Has exposure in the life estimation of the structure by using tool NASGRO.

• Has experience in writing programs by using PYTHON as well as in MATLAB.

• Has capability to independently review the stress analysis results and generate stress analysis reports.

• Good knowledge on carrying out LCF analysis for gas turbine.

• Good understanding of fatigue and fracture mechanics.

• Hands-on working experience in the areas of cold structure of turbofan engine of aircraft.

Domain Aero Engine and Automotive

Tool

Knowledge

CATIA V5, NX, HYPERMESH, SIMCENTER-3D, MSC NASTRAN, ANSYS WORKBENCH, APDL, ABAQUS, HYPERVEIW, NASGRO, PYTHON & MATLAB, TEAMCENTER

# Information Details

1. Employee Full Name SONIYA DEVI

2. Contact no. 789-***-****

3.

4.

Email ID

Location

adlkm9@r.postjobfree.com

Bangalore, India

4. DETAILED PROJECT EXPERIENCE

# Project Brief Description of the Project

Axiscades- Projects In Heavy Engineering Domain(OCT 2020 – March 2021) 1.

FE Modelling of D10

Retrieval, Roof Design,

ACP, Radiator, My

Camera, Cobraduct,

PCAP18Design, Tanks &

BJA

Analysis of 992 &996

Trucks

The work activity includes

• Mid Surface extraction.

• Geometry cleanup.

• Generation of Shell Meshing, Hexa and Tetra

Meshing, Weld split, Weld toe & Weld volume.

• Post processing of 992 & 996 trucks using

ABAQUS & HYPERVIEW.

• Preparation of report is done according to the

Customer standard using MS Office.

Axiscades - GKN Aerospace - Projects In Aero Engine Domain(July 2019 – Sept 2020) 2.

Stress tool development

for joints

• Collect required inputs for types of joints, Loads from the given database.

• Create the flowchart for each type of joint from the given database using PowerPoint.

• Write the program for each joint with help of

flowchart database using PYTHON for

evaluation of Allowable Stresses and Margin.

• Verification has been done with existing

database.

3.

Static strength analysis

of

MRJ 17K

• Collect required inputs like 3D Model, Loads

from the given database.

• Generate the FE Model and apply the loads.

• Change or create APDL script based on

requirement.

• Static strength analysis of the PW turbofan

engine of MRJ 17K.

• Limit, Ultimate, FBO, LCF, Windmilling Analysis

and DT Analysis as per TRS has been done using

ANSYS APDL,HYPERVIEW, NX, NASGRO,

PYTHON & MS-Office.

4.

Non Conformance

Support to BA 24K

• Study of inputs,

• Identify the component and location of the

defect with interaction of design department.

• Detailed study of the affected part /

component with the use of existing drawings

and Model

• Carried out Static Strength check of

component and LCF analysis.

• Create an APDL script for solving stress

concentration factor for common NC.

• Preparation of stress justification report using NX, HYPERVIEW, NASGRO & MS Office.

GBN Services - Projects in Automotive Domain(Sept 2014 – Dec 2016) 5.

FE Modeling and Modal

Analysis of Floor Panel and

Exhaust System

• FE Modelling of component by Mid surface

extraction and geometry cleanup.

Generation of shell and solid meshing with

welding of pipe and preparation of report

according to customer standard using

HYPERMESH, MSC NASTRAN & MS Office.

6.

FE Modeling of Door Trims

Assembly, B-Coros and

BIW Components

FE Modeling of the Door trims assembly. The work

activity includes

• Mid Surface extraction

• Geometry cleanup

• Generation of Shell Meshing

• Preparation of report is done according to

the Customer standard using HYPERMESH &

MS Office.

IIT Madras - MTech Project(May 2018 – May 2019)

6.

Modeling and Coupled

Analysis of UAV

● Modelling and detailed aerodynamic and

structural analysis of the air-frame of a medium

size (35kg) unmanned aerial vehicle(UAV) with

H-tail, twin-boom, pusher configuration IC

engine based power plant.

● 3D-modelling of various components of UAV

have been done and assembled using CATIAV5

for various simulations.

● CFD analysis have been done using ANSYS

FLUENT, PYTHON and analytically.

● Meshing and Structural analysis and of landing

gear and wing have been carried out using

ANSYS Workbench 18.1.

● Buckling check for wing structure have been

carried out using ANSYS Workbench 18.1.

● Meshing and Static analysis of chair of an UAV

has been carried ANSYS Workbench 18.1.

● Design changes have been proposed to ensure

better assembly and operational readiness based

on these analyses.

Center for Innovation, IITM LOCKHEED MARTIN’s Design Challenge (Aug 2017–June2018) 6.

FE Modeling and Analysis

of Chassis and

Components

● Conceptualize, Design, Manufacture & Test a

Cargo Carrier Vehicle for C130 Super

Hercules transport aircraft for loading and

unloading purpose.

● 1d,2d & 3d meshing, static analysis &

optimization of chassis and components have

been done to reduce the weight of Cargo Vehicle

using HYPERMESH, OPTISTRUCT & ABAQUS.

Course Project, IITM (Jan 2018 – Feb 2019)

6. Design and Fabrication

of Conventional UAV

● Design and fabrication of propeller

configuration small size(1.6 Kg)

conventional fixed wing UAV has been done

with team size (6 members).

● Aerodynamic design of UAV has been derived

for the given requirements and report

preparation using LATEX.

● 3D-modelling in CATIA V5 of Wing and H-tail

of UAV and evaluation of aerodynamic

parameters and stability derivatives of UAV as

well as structural analysis have been done

using ANSYS FLUENT, XFLR, MATLAB and

analytically.

Courses

● Flight Dynamics

● Aerospace Structure

● Aerospace Propulsion

● Aerodynamics and

Performance

● Design of MAVs and UAVs

● Composite Structure

● Failure Analysis and Design

● Design with advanced engineering Material

Position of Responsibility

● Mentored few BE students in area of Aerodynamics, Aircraft Structure from Jan 2017 to June 2017.

● Member of Space Development Nexus from Jan 2016 to June 2017.

● Coordinated in Sarang Jan 2018 at IIT Madras.

● Coordinated as Super-coordinator with Research Expo and Workshops Teams in RSD Feb 2019 at IIT Madras.

Contact this candidate