SANGEETHA S NAIR PH: +91-956*******

KOTHAKULUM 080********(office number)

KURUMPANADOM.P.O Email: admf4d@r.postjobfree.com PALAMATTOM

KOTTAYAM, KERALA

PIN: 686536

OBJECTIVE

To pursue a challenging carrier in the field of Aeronautical Engineering in a progressive way that gear up me scope to use my knowledge and skills to be a part of the them that excel in work can be utilized in an innovative and competitive world towards the developments of the personal growth along with the organization. TECHNICAL SKILLS

Under graduation,Aeromechanical Engineering (AeSI) Graduated, February 2017 Visveswaraya institute of engineering technology Marks 63%(First Division) The Aeronautical Society Of India.

Higher Secondary Education(HSE) Marks 75%

N.S.S Karukachal

Kerala

Matriculation(SSLC) Marks 95%

ST. Shantal’s H.S Mammood

Kerala

PROFESSIONAL SUMMARY

As part of the On Job Trainee program of the Aeronautical Society of India, I was appointed as an on Job Trainee at the Gas Turbine Research Establishment (GTRE) a lab operating under DRDO. 1. GAS TURBINE RESEARCH ESTABLISHMENT

Duration: 1 year (2017-2018)

Designation : Design Engineering Trainee

Division: RSIF (Rotary Supporting Integrating System of Fan) RESPONSIBILITIES

To assist in design related studies of Kaveri engine and small turbofan system by 3D and 2D finite element Modeling of components of the rotary system of gas turbine post processing analysis and Technical documentation. TRAINING DETAILS

2D Model Generation

Creation of 2D Models of small turbofan engine and Kaveri engine parts by using AutoCAD Name of Small Turbofan Engine Parts (2D Modeling)

Outer Cover, Extension Shaft Front Compressor, LPT Shaft, Ring Carbon Seal. Name of Kaveri Engine Parts (2D Modeling)

Mounting Bracket, Oil Sleeve, Extension shaft front compressor, Bus sump oil tank, Casing carbon seal. Modeling & Drafting : AutoCAD (2D Modeling), Unigraphics(UG-NX), CATIA V5 (3D Modeling) Pre & Post Processing : HyperMesh

Documentation : MS-Word, Excel, Power Point

Platforms : WIN7, WIN8

Programing language : C, C++, MATLAB

ACADEMIC CREDENTIALS

3D Model Generation and Drafting

Creation of 3D Models of STFE and Kaveri engine parts by using unigraphics (UG-NX) Name of Kaveri Engine Parts (3D Modeling)

Front cover No.5 BRG outer race, Oil Sleeve, Mounting Bracket, Nut Retainer, Extension shaft front compressor. Name of Small Turbofan Engine Parts (3D Modeling)

Extension shaft front compressor, Ring Carbon seal, Casing carbon seal, Hex- Slotted Screw MJ5X-8 Spacer Ring, Elastic Ring Axial Rotor disc, LP Front shaft, Roller Bearing, Locking Plate, LPT Disc.

FE Model Generation OF Small Turbo Fan Engine

Creation of FE Mesh of the small turbo fan engine parts like seal housing, Air adaptor Oil, Chamber Anti-icing Top and Bottom Compound,Nut Retainer,Different type of Casing intermediate and Bracket Mounting, Gearbox .By using hyper mesh and Von misses stress analysis by using ANSYS Workbench.

2. AERONAUTICAL DEVELEPMENT ESTABLISHMENT

Duration: 8-oct-2018 – Till Now

Designation : Contract Engineer

Division: FMC (Flight Mechanics control)

FMC division mainly doing Real time simulation and hardware in loop simulation. RESPONSIBILITIES

To assist Flight Mechanics Studies of Unmanned aerial vehicle by using 6DoF (Six Degree of Freedom) Simulation Model. WORK DETAILS

Flight Mechanics analysis for Store Separation (Payload release) of Lakshya-2 through Simulation.

Post Flight data analysis of Lakshya-2.

Lakshya-2 using different engines likes HAL engine and Micro turbo engine. Comparison of engine performance with help of MATLAB plotting tool.

Aero data implementation of different Unmanned aerial vehicles in 6DoF Model and Linear model and statics response Validation with aero data through Simulation.

Developed and updated Six degree of freedom model (6DoF) Mini Unmanned aerial vehicle (scale down model) implementing the Aerodynamic data, Structural data, Engine data.

Flight Mechanics studies of various Unmanned aerial vehicle and analysis have been carried out in various phase of flight through 6Dof simulation.

PROJECT

TITLE: Study of Supersonic Wind Tunnel: The objective was to understand the operation of various supersonic wind tunnels, the detailed study of supersonic wind tunnels includes the need for wind tunnels, different types of supersonic wind tunnels, their advantages and disadvantages:

ACADEMIC ACHEVEMENT

Undergone 6 Weeks Mechanical Work Shop Training Such as Fitting Shop, Foundry Shop And Machine Shop From Visveswaraya Institute Of Engineering Technology.

Successfully Completed 6 weeks Training Program In Aerodynamics, Propulsion,Sturcture Engines And Systems In The Laboratories Of The Department Of Aeronautical Engineering In, Mount Zion Collage of Engineering Pathanamthitta

(Approved by AICTE and affiliated to M.G University). PERSONAL DOSSIER

Name: Sangeetha S Nair Permanent Address: Kothakulum Father’s Name: Sajeev Kumar Kurumpanadom.P.O

Date of Birth : 15-10-1993 Palamattom

Marital status : Single Kottayam, Kerala

Nationality: Indian PIN: 686536

REFERENCE

Dr. T. Venkatakrishnaiah

Former Emeritus Scientist

Gas Turbine Research Establishment, DRDO

Email: admf4d@r.postjobfree.com

Ph. +91-990*******

DECLARATION

I hereby declare that the above mentioned details are true to the best of my knowledge. I offer myself as a candidate for your consideration.

Sangeetha s Nair

Date : 11-10-2020

Place: Bengaluru

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