PG

Pradeep Gupta

Indian Institute of Science, National Institute of Technology Agartala

ORCID iD 0000-0002-4032-5438
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About

I am a dedicated, hardworking, and ambitious Mechanical and Aerospace Engineer with a strong background in designing and carrying out experiments. I possess excellent analytical and communications skills and a dedicated approach to working in a highly controlled working environment. I am currently looking for an opportunity to utilize my technical skills in a challenging working environment.

Employment

Employment history is unavailable.

Education

  • Indian Institute of Science Post Doctoral Fellow
    2021 - Present
  • Indian Institute of Science PhD
    2016 - 2021
  • Indian Institute of Science M.E.
    2014 - 2016
  • National Institute of Technology Agartala B.Tech
    2010 - 2014

Projects & Funding

Projects & funding information is unavailable.

Publications (9)

  • Performance Evaluation of Air Ejectors using Artificial Neural Network Approach
    7th National and 1st International Conference Refrigeration and Air Conditioning NCRAC 2022 2022
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  • Artificial neural network model for single-phase real gas ejectors
    Applied Thermal Engineering 2022
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  • Numerical Studies of a supersonic Air Ejector using Large Eddy Simulation
    6th National and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras 2021
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  • Numerical Analysis of Ejector Performance Near the Critical Back Pressure
    National Symposium on Shock Waves 6, IIT Madras 2020
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  • NUMERICAL STUDIES ON THE TRANSITION FROM THE CRITICAL TO THE MIXED FLOW REGIME IN A CONSTANT AREA EJECTOR
    5th National and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 26-30, 2021, IIT Roorkee 2019
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  • Experimental investigations on mixing characteristics in the critical regime of a low-area ratio supersonic ejector
    Physics of Fluid 2019
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  • Effect of Duct Geometry on Mixing Characteristics in Constant Area Supersonic Ejector
    National Symposium on Shock Waves, TBRL Chandigarh 2018
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  • Artificial Neural Network Based Shape Optimization of Supersonic Ejectors in the Critical Flow Regime
    Applied Thermal Engineering
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  • Effect of Mixing Duct Geometry of Supersonic Ejector in the Critical Flow Regime
    Conference: International Symposium of Shock Wave 32: Singapore
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