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junned afsar basha s n

Aircraft stress engineer at INFOSYS

Shivamogga

5+ years of work experience

Infosys
Jan 20251 yr 10 mosPresent

Mysore

● Worked on Airbus A350 Fuselage Section 15 Skin-stringer team for different load loops – 1000 PDS, 1000 Freighter and 1000 ULR. ● Worked on both Metallic and composite parts static analysis. ● Exposed to different ISAMI analysis – Filled hole (Both MFH & CFH) , Damage tolerance, Plain strength, System hole penetration (static and buckling) and so on by using GFEM and DFEM models, ● In Skin-Stringer component worked on different Modules like FLS- forward lower shell, LJP- Lower junction panel, CP- Crown panel, LP- Lateral panel. ● Exposed to Preparing Statement of Work (SOW) and Dossiers of various skin-stringer modules. ● Have exposure on Airbus PASS and Enovia VPM. ● Have exposure on Concessions – over sanding.
Infosys
Jan 20241 yr 1 moJan 2025

Mysore, Karnataka, India

Bangalore Aircraft Industries Pvt. Ltd.
Dec 20212 yrs 1 moDec 2023

Maruti Suzuki India Limited
Jun 20191 yr 1 moJun 2020

junned’s AI Stack

gemini
gemini
ChatGPT
ChatGPT
Microsoft Copilot
Microsoft Copilot

Education

Visvesvaraya Technological University

Bachelor's degree, Mechanical Engineering

Visvesvaraya Technological University

20124 yrs2016

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junned afsar basha s n on Tal

Headline

Aircraft stress engineer at INFOSYS

About

A mechanical engineer who loves to stimulate real world scenarios in finite element modelling softwares like PATRAN, NASTRAN, HYPERMESH , ISAMI and check the aircraft components whether they are safe or not. which describes the safety of the aircraft.

Location

Shivamogga

AI stack

gemini

ChatGPT

Microsoft Copilot

Work experience

Senior System Engineer at Infosys, Jan 2025 - Present · 1 yr 10 mos, Mysore, ● Worked on Airbus A350 Fuselage Section 15 Skin-stringer team for different load loops – 1000 PDS, 1000 Freighter and 1000 ULR. ● Worked on both Metallic and composite parts static analysis. ● Exposed to different ISAMI analysis – Filled hole (Both MFH & CFH) , Damage tolerance, Plain strength, System hole penetration (static and buckling) and so on by using GFEM and DFEM models, ● In Skin-Stringer component worked on different Modules like FLS- forward lower shell, LJP- Lower junction panel, CP- Crown panel, LP- Lateral panel. ● Exposed to Preparing Statement of Work (SOW) and Dossiers of various skin-stringer modules. ● Have exposure on Airbus PASS and Enovia VPM. ● Have exposure on Concessions – over sanding.

System Engineer at Infosys, Jan 2024 - Jan 2025 · 1 yr 1 mo, Mysore, Karnataka, India

Asistant structural engineer at Bangalore Aircraft Industries Pvt. Ltd., Dec 2021 - Dec 2023 · 2 yrs 1 mo

Service Advisor at Maruti Suzuki India Limited, Jun 2019 - Jun 2020 · 1 yr 1 mo

Education

Bachelor's degree, Mechanical Engineering, Visvesvaraya Technological University

junned afsar basha s n - Senior System Engineer in Shivamogga | Tal