Aaditya Wangikar

Design Engineer I - Aerodynamics at NewSpace Research and Technologies
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Contact Information
us****@****om
(386) 825-5501
Location
Bengaluru, Karnataka, India, IN
Languages
  • English Elementary proficiency
  • Marathi Native or bilingual proficiency
  • Gujarati Native or bilingual proficiency
  • Hindi Elementary proficiency
  • Sanskrit Elementary proficiency
  • Kannada Elementary proficiency
  • German -

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Azan Parmar

Rarely one comes across someone with as much drive as Aaditya. I had the pleasure of sharing my time with Aaditya during our post graduation at IITK. He was been prolific in problem solving on Aerodynamics fundamentals and applicative problems. He has an acumen for optimizing the path way to a solution, be it via coding or analytical. I was amazed to know that apart from being knowledgeable on Aerodynamics, Aaditya has appreciable management and leadership skills, something that takes some years to come by. Aaditya would be a valuable asset to any team!

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Credentials

  • Aerospace Masterclass : Aircraft Design
    Udemy
    Nov, 2022
    - Nov, 2024
  • Deep Learning with PyTorch: Image Segmentation
    Coursera
    Oct, 2022
    - Nov, 2024
  • Fundamentals of Fluid Structure Interactions
    École Polytechnique
    Oct, 2022
    - Nov, 2024
  • Python for Data Visualization: Matplotlib & Seaborn
    Coursera
    Oct, 2022
    - Nov, 2024
  • 2022 Python for Machine Learning and Data Science Masterclass
    Udemy
    Aug, 2022
    - Nov, 2024
  • Deep Learning OnRamp
    MathWorks
    Aug, 2022
    - Nov, 2024
  • Machine learning with MATLAB
    MathWorks
    Aug, 2022
    - Nov, 2024
  • OPENFOAM From modeling to Programming
    Udemy
    Aug, 2022
    - Nov, 2024
  • Optimization OnRamp
    MathWorks
    Aug, 2022
    - Nov, 2024
  • Simulink OnRamp
    MathWorks
    Jul, 2022
    - Nov, 2024
  • MATLAB Fundamentals
    MathWorks
    Sep, 2021
    - Nov, 2024
  • Glider design performance and stability
    Udemy
    Aug, 2021
    - Nov, 2024
  • Particle Physics
    University of Geneva
    Sep, 2020
    - Nov, 2024
  • Astro 101: Black Holes
    University of Alberta
    Aug, 2020
    - Nov, 2024
  • Machine Learning for All
    University of London
    Aug, 2020
    - Nov, 2024
  • Sports and Building Aerodynamics
    Eindhoven University of Technology
    Aug, 2020
    - Nov, 2024
  • Statistical Thermodynamics
    University of Colorado Boulder
    Aug, 2020
    - Nov, 2024
  • Astronomy: Exploring Time and Space
    University of Arizona
    Jul, 2020
    - Nov, 2024
  • Machine Design - I
    Georgia Institute of Technology
    Jul, 2020
    - Nov, 2024
  • Programming for Everybody Getting started with Python
    University of Michigan
    Jul, 2020
    - Nov, 2024
  • Python Data Structures
    University of Michigan
    Jul, 2020
    - Nov, 2024
  • Introduction to Rocket Propulsion
    NPTEL
    Oct, 2019
    - Nov, 2024
  • Computational Fluid Dynamics
    NPTEL
    Apr, 2019
    - Nov, 2024
  • Matlab Programming for Numerical Computation
    NPTEL
    Mar, 2019
    - Nov, 2024
  • Introduction to Finite Volume Methods 1
    NPTEL
    Oct, 2018
    - Nov, 2024
  • STK Certification Level 1
    AGI (Analytical Graphics, Inc.)
    Jun, 2018
    - Nov, 2024

Experience

  • NewSpace Research and Technologies
    • India
    • Aviation & Aerospace
    • 200 - 300 Employee
    • Design Engineer I - Aerodynamics
      • Jul 2023 - Present

  • Indian Institute of Technology, Kanpur
    • India
    • Higher Education
    • 700 & Above Employee
    • Postgraduate Student
      • Jul 2021 - Present

    • Teaching Assistant
      • Aug 2022 - Jul 2023

      Teaching Assistant for the course TA101 : Engineering Drawing

  • Indian Institute of Science (IISc)
    • India
    • Research
    • 700 & Above Employee
    • Project Intern
      • Mar 2021 - Jul 2021

      Multidisciplinary work involves design and optimization of conceptual air breathing hypersonic vehicle. Four different modules - Aerodynamics, Aerodynamics, Thermo-Structures and Stability were designed and analysed using MATLAB. Scramjet integrated waverider was designed using Stream Thrust Analysis. Forebody of the vehicle was designed using oblique shock relation. Combustion unit was designed using Turbulent shear mixing relationship and generalised ODE for heat addition with increasing area for constant pressure. Nozzle was designed using Method of characteristics. Thermostructural analysis was carried out by calculating aerodynamic heat flux and subsequently determining the equilibrium wall temperature for given thickness amd material. Waverider concepts were incorporated in integration of the vehicle and subsequently shock expansion method was used to calculate aerodynamic forces acting on the vehicle. Stability analysis was performed to calculate position orientation and shape of the stabilizer. Various parameters were identified and parameterization was performed linking input and output parameters. NSGA and ANN concepts was used to build surrogate model which is used for optimisation of the vehicle. Show less

  • Team Antariksh
    • India
    • Aviation and Aerospace Component Manufacturing
    • 1 - 100 Employee
    • Chief Subsystem Engineer, Aerodynamics Subsystem
      • Aug 2019 - Aug 2020

    • Sponsorship Marketing and Publicity
      • May 2018 - Aug 2020

    • Thermal Subsystem Engineer
      • Jan 2018 - Apr 2019

  • ELEATION
    • India
    • Mechanical Or Industrial Engineering
    • 1 - 100 Employee
    • Intern
      • May 2019 - Jun 2019

      Skills: CAE Software: ANSYS Skills: CAE Software: ANSYS

Education

  • Indian Institute of Technology, Kanpur
    Master of Technology - MTech, Aerospace Engineering /Aerodynamics
    2021 - 2023
  • R. V. College of Engineering, Bangalore
    Bachelor of Engineering - BE, Aerospace engineering
    2017 - 2021
  • Bharatiya vidya bhavans, Vadodara
    High School
    2014 - 2016
  • Bright Day School Vadodara
    School
    2006 - 2014

Community

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