Engineer Engineering

Shivakumar S Gonal

Aeronautical Engineer

Competent and dynamic engineer with 5+ years of experience in the field of finite elements and fluid dynamics. *****.*****@*****.*** 916-***-**** Bengaluru - 102, India EDUCATION

M. Tech - Aeronautical Engineering

MVJ College of Engineering

09/2013 - 08/2015, Bengaluru

B. E - Aeronautical Engineering

SCT Institute of Technology

09/2009 - 07/2013, Bengaluru

WORK EXPERIENCE

Engineer II

Safran Engineering Services

08/2018 - Present, Bengaluru

Geometry clean up, grid generation and preparation of input decks for Non-linear and Computational Fluid Dynamics activities.

Hands on experience in the field of Bird ingestion and Fan blade out studies.

Performance evaluation of flow past fan blade at

different speeds, pitch angles & tip clearances at

different throttle points through computational fluid dynamic approach.

Aeronautical Engineer

Aeronautical Development Agency

09/2015 - 08/2018, Bengaluru

Nonlinear analysis and transient CFD simulations on different parts of LCA aircraft.

Problem setup and validation of bird impact on

windscreen and air intake.

Arrester barrier engagement simulation of LCA

aircraft with or without refueling probe, with or

without drop ranks.

Transient CFD activities include slosh and vibration simulation of different LCA drop tanks.

SKILLS

LS-Prepost LS Dyna HYPERMESH Samcef

ANSYS Fluent CFD-Post Autogrid

Cannelle elsA SpaceClaim

Fluent Meshing SU2 PARAVIEW Python

ACADEMIC PROJECTS

Accurate Drag Computation and Decomposition

from CFD solutions from Mid Field method

An independent MFDD code has been developed to

compute each physical drag components such as viscous, wave, induced and spurious components; latter is due to the numerical dissipation and truncation errors, in order to estimate the accurate drag coefficient values

NAL, Bengaluru

Design and Optimization of UAV Winglet

This study involves modeling and steady state analysis of a typical UAV wing with and without winglet. Grid convergence study, Iterative convergence studies, Turbulence Model testing and validation with experimental results,

optimization of the winglet have been carried out by varying cant angles and taper ratios of winglet

IISc., Bengaluru

CERTIFICATES

Coding in Computational Fluid Dynamics

(07/2015 - 08/2015)

AlphaTech Center, Bengaluru

Introduction to Numerical grid generation and

fluid flow computations (08/2014 - 12/2014)

IISc, Bengaluru

In-Plant Training (01/2012 - 02/2012)

HAL, Engine Division, Bengaluru

LANGUAGES

Kannada

English

Hindi

PAPERS

2 Journals 3 Conference Ppapers

Workflow

Workflow

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