Jatinder Pal Singh Sandhu

About

I am a researcher with an interest in the field of computational fluid dynamics (CFD). My recent work involves the development and analysis of a laminar-to-turbulent flow transition model. Additionally, I have worked on a few high-speed passive flow control devices, such as vortex generators and porous mediums, with an application to transonic and supersonic flights. I have also worked on the numerical/algorithm aspect of CFD, such as improving a steady-state solution's convergence.

Employment

• Yanxiki Tech. Senior R&D engineer
  2022 - Present

Education

• Indian Institute of Technology Madras Ph.D.
  2015 - 2021
• National Institute of Technology Kurukshetra B.Tech
  2011 - 2015

Projects & Funding

Projects & funding information is unavailable.

Publications (12)

• Kriging-based multi-objective aerodynamic optimization of external compression supersonic intake
  Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2026 DOI: 10.1177/09544100251383692
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• Dynamical system analysis of a zero-equation transition model for sensitivity to initial conditions
  AIAA AVIATION 2021 FORUM 2021 DOI: 10.2514/6.2021-2724
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• Dynamical Systems Analysis of a Zero-Equation Transition Model
  AIAA Journal 2021 DOI: 10.2514/1.j060558
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• Drag reduction in transonic shock-wave/boundary-layer interaction using porous medium: a computational study
  Shock Waves 2021 DOI: 10.1007/s00193-021-01009-7
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• A local correlation-based zero-equation transition model
  Computers and Fluids 2021 DOI: 10.1016/j.compfluid.2020.104758
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• FEST-3D: Finite-volume Explicit STructured 3-Dimensional solver
  Journal of Open Source Software 2020 DOI: 10.21105/joss.01555
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• Local-Correlation Based Zero-Equation Transition Model for Turbomachinery
  Proceedings of the ASME 2019 Gas Turbine India Conference. Volume 1: Compressors, Fans, and Pumps; Turbines; Heat Transfer; Structures and Dynamics 2020 DOI: 10.1115/GTINDIA2019-2615
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• A simplified local correlation-based zero-equation transition model
  AIAA AVIATION 2020 FORUM 2020 DOI: 10.2514/6.2020-2992
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• Effectiveness of micro-vortex generators in tandem in high-speed flows
  AIAA AVIATION 2020 FORUM 2020 DOI: 10.2514/6.2020-2961
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• Evaluation of Ramp-Type Micro Vortex Generators Using Swirl Center Tracking
  AIAA Journal 2018 DOI: 10.2514/1.j056796
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