DANIEL GUGGENHIEM SCHOOL OF AEROSPACE ENGINEERING, GEORGIA TECH, ATLANTA, USA

• Playing a key role in instructing, advising and supporting 40+ upperclassmen in understanding the experimental and applied physical concepts on Introductory experimental methods in Aerospace Engineering

• Assisted in developing and reconfiguring Arduino experimental kits as a replacement for dated equipments helping in 

• Researching on novel shape parametrization algorithms and design optimization study with AI integration for physically meaningful airfoil parametrization and flow field computation

SPACE TRANSPORTATION SYSTEMS ENGINEERING LABORATORY (VIRTUAL), KYUSHU UNIVERSITY, JAPAN

• Implemented GUI less FLUENT - MATLAB flow computation framework with industry standard PARSEC airfoil parametrization algorithm for airfoil shape generation

• Developed data-driven higher order Deep learning model with reduced order model integration for accurate and efficient flowfields reconstructions in transonic regime.

• Researching on novel shape parametrization algorithms and design optimization study with AI integration for physically meaningful airfoil parametrization and flow field computation

MANIPAL INSTITUTE OF TECHNOLOGY, MANIPAL, KARNATAKA, INDIA

• 1st Student to be selected as TA for the department of aeronautical engineering at UG level

• Managed a class of 40+ students and responsible for teaching, evaluation and syllabus making for the Numerical Computation Lab.

DEFENCE RESEARCH AND DEVELOPMENT LABORATORY (DRDL), HYDERABAD, INDIA

• Qualified among a diverse pool of applicants for highly competitive and selective Hypersonic missile development program internship

• Developed 3+ high fidelity algorithm governed by existent numerical schemes to capture the boundary layer effects due to shock formation

UNIVERSITY OF ILLINOIS, URBANA CHAMPAIGN - UIUC  (VIRTUAL), ILLINOIS, USA

• Worked on python code to model ionization and reaction of atmospheric gases

• Acquired understanding on the on the Non-Equilibrium Statistical Thermodynamics for development of Reduced order state-to-state solver for hypersonic reentry condition

THE DIGITAL DARWIN (DD), MANIPAL, KARNATAKA, INDIA

• A fledgling tech startup aimed at creating tailored VR/AR teaching assistive tools and experiences for next generation human training requirements

• Created 4+ MVP and developed novel hardware solution for classroom integration

REDON SYSTEMS PVT. LTD (VIRTUAL), HYDERABAD, TELANGANA, INDIA

• Worked on computational and numerical analysis of the firm's concept trainer aircraft by incorporating time marching viscous schemes for low altitude operation

CURIOUZ TECHLABS, MANIPAL, KARNATAKA

• Designed a completely sustainable easily deployable  “waterless urinal”  as a solution to the ever growing Indian-urban sanitization needs and to promote as a preferable alternative for unhygienic open space urination. 

• Noteworthy features: Sustained powering through Vertical Axis Wind Turbine , Solar panels to name a few; Hand sanitization, penis sleeve and vagina cup system (under patent) to facilitate hygienic urination for the old age

SPACE TECHNOLOGY & AERONAUTICAL ROCKETRY - STAR (VIRTUAL), SURAT, GUJARAT, INDIA

• Designed an advanced light High-power Rocket non pyro ejection system coupled with lossless Arduino based data acquisition, processing and transmission.

COLLEGE OF AVIATION TECHNOLOGY (VIRTUAL), DHAKA, BANGLADESH

• Initiated and worked on an ambitious self-sustaining Martian Settlement design project for 10000 civilians in Hellas Planitia. Design study involves deploying a state of the art ETFE and inflatable habitat duo with the fractal configuration for potential expansions in the future

• Key considerations were laid on the infrastructure for radiation and dust resilience, safety and for maintaining human psychology in distant lands.

HINDUSTAN AERONAUTICS LIMITED (HAL), BANGALORE, KARNATAKA, INDIA

• Acquired familiarization on the aerodynamic principles of the helicopter and utilization of rotorcrafts in defence applications.  Applied the learnings in developing a MATLAB code snippet for rudimentary panel method based flow parameters computation.

• Gained extensive knowledge on team coordination and management and understood functioning of other disciplines of rotorcraft production such as avionics, structural, thermodynamics, and propulsion divisions,