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Prince Raj Lawrence Raj

About


I have joined IIESTS in April 2019. Prior to that, I was working as a researcher for one year and six months with Research Center for Aircraft Core Technology, Gyeongsang National University, South Korea. I did my Ph.D. from the Department of Mechanical and Aerospace Engineering, Gyeongsang National University, South Korea. During my Ph.D., I studied fluid dynamics theories, mathematical modeling of droplet physics and atmospheric icing physics, numerical modeling of various partial differential equations (PDE), parallel computation, and various applications on aircraft. In particular, I focused on the mathematical modeling of supercooled large droplet impingement behavior and ice accretion on the aircraft surface. Further, my research was expanded to the simulation of high-speed flows and rarefied gas dynamics. Moreover, a few of my research was focused on the implementation of parallel computation for the Discontinuous Galerkin Method (DGM) and FVM. My research interests are in the broad areas of mathematical modeling and simulation applied to the field of fluid dynamics, multiphase flow, heat transfer, icing physics, hypersonic flows, and parallel computation.

Academic Qualifications


  • Doctor of Philosophy in Aerospace Engineering (2017), Gyeongsang National University, South Korea.
  • Master of Technology in Aeronautical Engineering (2011), Anna University of Technology, Tirunelveli.

Research Statement


Learning by doing is the best way of conducting research.

Latest Publications


  • 1 Sung Ki Jung, L. Prince Raj, A.Rahimi, H.Jeong, R.S.Myong, Performance evaluation of electrothermal anti-icing systems for a rotorcraft engine air intake using a meta model, Aerospace Science and Technology, 2020
  • 2 Raj, L Prince and Yee, K and Myong, RS, Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing, 105659, Aerospace Science and Technology, 2020
  • 3 Raj, Prince Raj Lawrence and Jeong, Hojin and Roy, Rene and Kweon, Jin-Hwe and Myong, Rho Shin, Computational Simulation of an Electrically Heated Ice Protection System for Composite Leading Edges of Aircraft, SAE Technical Paper, 2019
  • 4 Lawrence Raj, Prince Raj and Myong, Rho Shin, Three-Dimensional Computational Simulation of Glaze Ice Accretion on a Rotorcraft Engine Intake, 1659, AIAA Scitech 2019 Forum, 2019
  • 5 Raj, L Prince and Lee, JW and Myong, RS, Ice accretion and aerodynamic effects on a multi-element airfoil under SLD icing conditions, 85, 320--333, Aerospace Science and Technology, 2019
  • 6 Sengupta, Bidesh and Cho, Min Young and Raj, Lawrence Prince and Myong, Rho Shin, Development of Aero and 6-DOF Solvers for Predicting Ice Shedding Trajectory, 54--55, Korean Society for Aeronautical and Space Sciences, 2019
  • 7 Jo, J H and Raj, L Prince and Lee, Y M and Lee, J H and Myong, R S, Computational Analysis of Ridge Iced Airfoil Flow Field Using RANS and LES, 24, 8--18, Journal of Computational Fluids Engineering, 2019
  • 8 Raj, L Prince and Vaghela, M and Myong, RS, COMPUTATIONAL INVESTIGATION OF EFFECTS OF ROUGHNESS AND HEAT TRANSFER ON AIRFOIL ICE ACCRETION, 140--141, Korean Society for Aeronautical and Space Sciences, 2018
  • 9 Mondal, T and Raj, L Prince and Myong, RS, NUMERICAL INVESTIGATION OF CONJUGATE HEAT TRANSFER OF TWO IMPINGING JETS FOR ANTI-ICING OF AIRCRAFT, 150--151, Korean Society for Aeronautical and Space Sciences, 2018
  • 10 L. Prince Raj and S. Singh and A. Karchani and R.S. Myong, A super-parallel mixed explicit discontinuous Galerkin method for the second-order Boltzmann-based constitutive models of rarefied and microscale gases, 157, 146-163, Computers & Fluids, 2017
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    Research Areas


    • Aircraft icing
    • High-Performance Computing
    • Hypersonic Flow
    • Computational Fluid Dynamics
    • Multiphase Flow
    • Aerodynamics
    • Heat Transfer

    Publications


    1 Sung Ki Jung, L. Prince Raj, A.Rahimi, H.Jeong, R.S.Myong, Performance evaluation of electrothermal anti-icing systems for a rotorcraft engine air intake using a meta model, Aerospace Science and Technology, 2020 2 Raj, L Prince and Yee, K and Myong, RS, Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing, 105659, Aerospace Science and Technology, 2020 3 Raj, Prince Raj Lawrence and Jeong, Hojin and Roy, Rene and Kweon, Jin-Hwe and Myong, Rho Shin, Computational Simulation of an Electrically Heated Ice Protection System for Composite Leading Edges of Aircraft, SAE Technical Paper, 2019 4 Raj, L Prince and Lee, JW and Myong, RS, Ice accretion and aerodynamic effects on a multi-element airfoil under SLD icing conditions, 85, 320--333, Aerospace Science and Technology, 2019
  • 5 Jo, J H and Raj, L Prince and Lee, Y M and Lee, J H and Myong, R S, Computational Analysis of Ridge Iced Airfoil Flow Field Using RANS and LES, 24, 8--18, Journal of Computational Fluids Engineering, 2019
  • 6 L. Prince Raj and S. Singh and A. Karchani and R.S. Myong, A super-parallel mixed explicit discontinuous Galerkin method for the second-order Boltzmann-based constitutive models of rarefied and microscale gases, 157, 146-163, Computers & Fluids, 2017
  • 7 Raj, LP and Myong, RS, Computational Analysis of An Electro-Thermal Ice Protection System in Atmospheric Icing Conditions, 21, 1--9, Journal of Computational Fluids Engineering, 2016
  • 8 Balu, R and Raj, L Prince, Analysis of Heat Transfer in Hypersonic Flow over Re-Entry Configurations, 3, 1--10, International Journal of Advances in Thermal Sciences and Engineering, 2012
  • 1 Lawrence Raj, Prince Raj and Myong, Rho Shin, Three-Dimensional Computational Simulation of Glaze Ice Accretion on a Rotorcraft Engine Intake, 1659, AIAA Scitech 2019 Forum, 2019
  • 2 Sengupta, Bidesh and Cho, Min Young and Raj, Lawrence Prince and Myong, Rho Shin, Development of Aero and 6-DOF Solvers for Predicting Ice Shedding Trajectory, 54--55, Korean Society for Aeronautical and Space Sciences, 2019
  • 3 Raj, L Prince and Vaghela, M and Myong, RS, COMPUTATIONAL INVESTIGATION OF EFFECTS OF ROUGHNESS AND HEAT TRANSFER ON AIRFOIL ICE ACCRETION, 140--141, Korean Society for Aeronautical and Space Sciences, 2018
  • 4 Mondal, T and Raj, L Prince and Myong, RS, NUMERICAL INVESTIGATION OF CONJUGATE HEAT TRANSFER OF TWO IMPINGING JETS FOR ANTI-ICING OF AIRCRAFT, 150--151, Korean Society for Aeronautical and Space Sciences, 2018
  • 5 Raj, L Prince and Jang, WY and Myong, RS, EULERIAN-BASED SIMULATION OF DROPLET IMPINGEMENT ON THE ENGINE INLET NACELLE, 112--113, Korean Society for Aeronautical and Space Sciences, 2017
  • 6 Mondal, T and Raj, L Prince, NUMERICAL INVESTIGATION OF INTERACTION OF TWO TURBULENT PARALLEL JETS WITH VARIOUS VELOCITY RATIOS, 39--40, Korean Society for Aeronautical and Space Sciences, 2017
  • 7 L. Prince Raj, R.S. Myong, Numerical Simulation of Droplet Impingement on a Multi-Element High-Lift Airfoil, International Council of the Aeronautical Sciences, (ICAS 2016), 2016
  • 8 Raj, L Prince and Singh, S and Karchani, A and Myong, RS, PARALLELIZATION OF A MODAL DISCONTINUOUS GALERKIN METHOD USING SPMD PROGRAMMING MODEL, 160--161, Korean Society for Aeronautical and Space Sciences, 2016
  • 9 Raj, L Prince and Jung, SK and Myong, RS, A FINITE VOLUME METHOD FOR 3-D DROPLET IMPINGEMENT IN SUPERCOOLED LARGE DROPLET ICING CONDITIONS, 267--268, Korean Society for Aeronautical and Space Sciences, 2014
  • 10 Raj, LP and Myong, RS, A FINITE VOLUME METHOD FOR SIMULATION OF SUPERCOOLED LARGE DROPLETS IN ATMOSPHERIC ICING, 171--172, Korean Society for Aeronautical and Space Sciences, 2014
  • 11 Raj, L Prince and Rejith, P and Balu, R, Numerical simulation of a hot gas injection thrust vector control system performance, 38, 1745--1749, Procedia Engineering, 2012
  • Patents


    # Patents Year

    Created: 23 November 2019