Chetan Mistry

About

Dr.Chetan S. Mistry is an Associate Professor in the Department of Aerospace Engineering, IITKharagpur.He has 22 years’ experience in teaching and research. He has done his graduation in Mechanical Engineering from REC, Surat (Presently NIT-Surat). He received his Master’s of Engineering in Turbo Machinery from NIT, Surat; Ph.D. from IIT Bombay. His Ph.D. thesis on “Experimental Investigation on the Performance of a Contra Rotating Fan Stage under Clean and Distorted Inflow Conditions” awarded with “Award for Excellence in Thesis Work”, IIT Bombay in 2014. He is also a recipient of “ASME- IGTI-Young Engineer Travel Award” in 2013. His area of research are: design and performance augmentation strategies for turbomachines, experimental and CFD study of turbomachines, contra rotating axial flow turbomachines aerodynamics, electric propulsion as well as fluid mechanics & heat transfer, and experimental aerodynamics.

Employment

• Indian Institute of Technology Kharagpur Associate Professor
  2026 - Present
• Indian Institute of Technology Kharagpur Assistant Professor
  2016 - Present
• Indian Institute of Technology Kharagpur Assistant Professor
  2016 - 2026

Education

• Indian Institute of Technology Bombay PhD
  2010 - 2014

Projects & Funding

Projects & funding information is unavailable.

Publications (33)

• Numerical Modelling of Wind Tunnel Internal Flow for CFD Assisted Design
  Journal of The Institution of Engineers (India): Series C 2024 DOI: 10.1007/s40032-021-00794-5
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• Characterization of Leading-edge Laminar Separation Bubble for various Angles of Incidence and Reynolds Numbers
  Journal of The Institution of Engineers (India): Series C 2024 DOI: 10.1007/s40032-022-00831-x
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• Effect of axial extension on parameterized endwall contour with incidence change for low-pressure turbine linear cascade
  Journal of Mechanical Science and Technology 2023 DOI: 10.1007/s12206-023-2109-7
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• Numerical Investigations on Effect of Inflow Parameters on Development of Secondary Flow Field for Linear Low-Pressure Turbine Cascade
  Journal of Turbomachinery 2023 DOI: 10.1115/1.4056093
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• Development of time-efficient multi-hole pressure probe calibration facility
  Lecture Notes in Mechanical Engineering 2021 DOI: 10.1007/978-981-15-5039-3_18
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• Innovative Approach for Design and Development of Annular Sector Cascade Tunnel using Numerical Analysis
  Journal of The Institution of Engineers (India): Series C 2021 DOI: 10.1007/s40032-021-00770-z
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• NUMERICAL INVESTIGATIONS on EFFECT of INFLOW PARAMETERS on DEVELOPMENT of SECONDARY FLOW FIELD for LINEAR LP TURBINE CASCADE
  Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021 2021 DOI: 10.1115/GTINDIA2021-76008
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• Numerical Investigations on Application of Cantilever Stator on Aerodynamic performance of Tandem Bladed Axial-Flow Compressor
  Proceedings of the ASME Turbo Expo 2021 DOI: 10.1115/GT2021-60233
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• Numerical investigations on aerodynamic design criteria for low speed mixed flow compressor
  Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021 2021 DOI: 10.1115/GTINDIA2021-76013
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• Preface
  Lecture Notes in Mechanical Engineering 2021
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