Aerospace Engineering

• IGTI YOUNGENGINEERTRAVEL AWARD
• AWARD FOR EXCELLENCE IN THESIS

Book Chapter/Section
• Aerodynamic Design of Fan Rotors for Ultra-High-By-Pass-Ratio Turbofan Engines Ernesto B., Mistry C. S. By AIAA educational series book. - (Accepted/In-Press)
• Effect of Various Periodic Surface Concepts for Numerical Investigation of Flow Field Through Variable Area LP Turbine Nozzle Mistry C. S., Bhavsar H. By Proceedings of the National Aerospace Propulsion Conference 1-12 (2022)
Patent
• AXIAL-CENTRIFUGAL CONTRA-ROTATING LIGHT WEIGHT, COMPACT COMPRESSION SYSTEM. Mistry C. S., A. By - (Accepted/In-Press)
• AXIAL-CENTRIFUGAL CONTRA-ROTATING COMPRESSOR SYSTEM ADAPTED FOR HIGH THRUST TO WEIGHT RATIO OF GAS TURBINE ENGINE Mistry C. S., A. By - (2020)
Journal
• Understanding of tip clearance flow structure in high speed mixed flow compressor H., Mistry C. S. By Propulsion and Power Research 1-15 (Accepted/In-Press)
• Numerical Investigations on Effect of Inflow Parameters on Development of Secondary Flow Field for Linear Low-Pressure Turbine Cascade Darji A.P., Baloni B.D., Mistry C.S. By Journal of Turbomachinery 145 - (2023)
• Effect of Axial Extension on Parameterized Endwall Contour with Incidence change for LP Turbine Linear Cascade Darji A., Baloni B. , Mistry C. S. By Journal of Mechanical Science and Technology 37 2223-2322 (2023)
• Effects of total pressure distribution on performance of small size counter-rotating Axial-flow fan stage for electrical propulsion Mistry C. S., Bandopadhyay T. By ASME Open Journal of Engineering 1-14 (2022)
• Numerical Modelling of Wind Tunnel Internal Flow for CFD Assisted Design Kesharwani S., Mistry C. S., Roy S. , Roy A. , Sinhamahapatra K. P. By Journal of Institution of Engineers (India) Series C - (2022)
• Characterization of leading-edge laminar separation bubble for various angle of incidences and Reynolds numbers Mistry C. S., Bandopadhyay T. By Journal of The Institution of Engineers (India): Series C. , Springer 1-20 (2022)
• Structure and Vibration Analyses of Low Speed Contra-Rotating Fan Stage with High Aspect Ratio Mistry C. S., Ghosh A. , Sah S. By International Journal of Aerospace System Engineering 1-10 (2021)
• Structure and Vibration Analyses of Low Speed Contra-Rotating Fan Stage with High Aspect Ratio Mistry C. S., Ghosh A. , Sah S. By International Journal of Aerospace System Engineering 8 1-13 (2021)
• Innovative Approach for Design and Development of Annular Sector Cascade Tunnel Using Numerical Analysis Mistry C. S., Bhavsar H. By Journal of The Institution of Engineers (India): Series C 1-21 (2021)
• Propagation of Different Types of Inflow Distortions through a Contra Rotating Fan Stage Mistry, C.S. and Pradeep, A.M. By International Journal of Turbo and Jet Engines 32(1) 41-57 (2015)
• Experimental Investigation of a High Aspect Ratio, Low Speed Contra Rotating Fan Stage with Complex Inflow Distortion Mistry, C.S. and Pradeep, A.M. By Propulsion and Power Research Vol.3(2) 68-81 (2014)
• Experimental Investigation of the Effect of Radially Distorted Inflow on a Contra-Rotating Fan Stage Mistry, C.S. and Pradeep, A.M. By International Journal of Rotating Machinery Vol. 2014(2014) 1-15 (2014)
• Influence of Circumferential Inflow Distortion on the Performance of a Low Speed, High Aspect Ratio Contra Rotating Axial Fan Mistry, C.S. and Pradeep, A.M. By ransactions ASME, Journal of Turbomachinery Vol. 136 071009-1-11 (2014)
• Effect of Variation in Axial Spacing and Rotor Speed Combinations on the Performance of a High Aspect Ratio Contra Rotating Axial Fan Stage Mistry, C.S. and Pradeep, A.M., By Proc. of IMechE, Part A: Journal of Power and Energy Vol. 227 138-146 (2013)
• Comparative assessment on performance of multi-cylinder engine using CNG, LPG and petrol as a fuel Mistry, C.S. By SAE2005 Transactions Journal of Passenger Cars-Electronic & Electrical systems March-2006 1-6 (2005)
Educational Package
• Aerodynamic Design of Axial Flow Compressors & Fans Mistry C. S. By - (2022)
Edited Volume
• Recent Advances in Computational and Experimental Mechanics, Vol II Maiti D. K., Jana P. , Mistry C. S., Ghoshal R. , Afzal M. S., Patra P. K., Maity D. By Recent Advances in Computational and Experimental Mechanics, Vol II - (2022)
• Recent Advances in Computational and Experimental Mechanics, Vol I Maity D., Patra P. K., Afzal M. S., Ghoshal R. , Mistry C. S., Jana P. , Maiti D. K. By Recent Advances in Computational and Experimental Mechanics, Vol I - (2022)
Conferences
• Effect of Axial Extension on Parameterized Endwall Contour with Incidence change for LP Turbine Linear Cascade Darji A., Baloni B. D., Mistry C. S. By Asian Congress on Gas Turbines 2022 (ACGT2022) 1-12 (2022)
• Effects of head geometry on five-hole pressure probes for wide angular range Singh A., J. , Mistry C. S. By 4th National Aerospace Propulsion Conference (NAPC-2022) 1-10 (2022)
• Parametric study of DCA airfoil using MISES Mandal G., Mistry C. S. By 4th National Aerospace Propulsion Conference (NAPC-2022) 1-10 (2022)
• Parametric Study on Different Size of Circular Pivots in Part Clearance of Variable Area LP Turbine Nozzle Vane Bhavsar H., Mistry C. S. By 4th National Aerospace Propulsion Conference (NAPC-2022) 1-14 (2022)
• Passive flow control approach for design of wide angle diffuser of linear cascade tunnel Bhavsar H., Mistry C. S. By 4th National Aerospace Propulsion Conference (NAPC-2022) 1-12 (2022)
• Development of Curved Shape Diffuser-Duct for Aero-Engines with a Backend Centrifugal Compressor A., Mistry C. S., S. , Pratap A. By 4th National Aerospace Propulsion Conference (NAPC-2022) 1-14 (2022)
• Development of time-efficient multi-hole pressure probe calibration facility Singh A., Kumar A., Tayal G., Mistry C. By Lecture Notes in Mechanical Engineering 313-336 (2021)
• Numerical investigations on aerodynamic design criteria for low speed mixed flow compressor Kumar H., Mistry C.S. By Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021 - (2021)
• Numerical Investigations on Application of Cantilever Stator on Aerodynamic performance of Tandem Bladed Axial-Flow Compressor Mistry C. S., Singh A. , Talwar B. By ASME TurboExpo-2021 1-12 (2021)
• Numerical Investigations on Application of Cantilever Stator on Aerodynamic performance of Tandem Bladed Axial-Flow Compressor Tanwar B.P.S., Singh A., Mistry C.S. By Proceedings of the ASME Turbo Expo 2A-2021 - (2021)
• NUMERICAL INVESTIGATIONS on EFFECT of INFLOW PARAMETERS on DEVELOPMENT of SECONDARY FLOW FIELD for LINEAR LP TURBINE CASCADE Darji A.P., Baloni B.D., Mistry C.S. By Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021 - (2021)
• Aerodynamic design aspects for stator of highly loaded tandem bladed axial compressor Singh A., Mistry C.S. By Proceedings of the ASME Turbo Expo 2A-2020 - (2020)
• Numerical Analysis on Effect of Tip Clearance Flow for LP Turbine Linear Cascade Gedam A., M. , Bhavsar H. , Mistry C. S. By AeSI International Conference 1-8 (2020)
• Numerical investigations on the effect of pivot shapes in part clearance flow field of variable area LP Turbine nozzle vane Bhavsar H., Mistry C. S. By ASME Turbo Expo-2020 1-10 (2020)
• Effect of Various Periodic Surface Concepts for Numerical Investigation of Flow Field Through Variable Area LP Turbine Nozzle Mistry C. S., Bhavsar H. By National Aerospace Propulsion Conference (NAPC) 1-10 (2020)
• Extending the angular measurement range of a miniature 5-hole probe for measurements in turbomachines Singh A., A. , Bhavsar H. , Mistry C. S. By AeSI International Conference 1-10 (2020)
• Flow Study of Tandem Arrangement of Intakes at Take-off Condition for an Electrical Vehicle Mistry C. S., Sai Subhankar V. , A. , Surampally V. , Rathi D. , Bandopadhyay T. By National Aerospace Propulsion Conference (NAPC) 1-12 (2020)
• High Speed Turbo Pump Inducer Sensitive Response of Cavitating Flow, its Modulation and Challenges Mistry C. S., Akula P. By National Aerospace Propulsion Conference (NAPC) 1-7 (2020)
• Numerical performance and flow field study of centrifugal compressor with supercritical carbon-dioxide (SCO2) Kumar H., Mistry C.S. By ASME 2019 Gas Turbine India Conference, GTINDIA 2019 1 - (2019)
• Numerical study of part clearance and free stream turbulence on high end-wall Lp turbine nozzle annular cascade Bhavsar H., Mistry C.S. By ASME 2019 Gas Turbine India Conference, GTINDIA 2019 1 - (2019)
• Study on effect of axial overlap on tip leakage flow structure in tandem bladed low speed axial flow compressor Singh A., Mistry C.S. By Proceedings of the ASME Turbo Expo 2A-2019 - (2019)
• Parametric study for adoption of variable cycle engine concept for low bypass ratio turbofan engine Swaminathan K., Mistry C.S. By ASME 2019 Gas Turbine India Conference, GTINDIA 2019 2 - (2019)
• Effects of total pressure distribution on performance of small size counter-rotating axial-flow fan stage for electrical propulsion Bandopadhyay T., Mistry C.S. By ASME 2019 Gas Turbine India Conference, GTINDIA 2019 1 - (2019)
• DEVELOPMENT OF TIME EFFICIENT MULTIHOLE PRESSURE PROBE CALIBRATION FACILITY Singh A., A. , G. , Mistry C. S. By National AErospace Propulsion Conference - (2018)
• Structural and Vibration Analysis of High Aspect ratio Low Speed Contra-Rotating Fan Stage Sah S. K., Ghosh A. , Mistry C. S. By 7th The International Conference on Theoretical, Applied, Computational and Experimental Mechanics - (2017)
• Flow Studies On a Single Stage Transonic Axial Flow Compressor Retrofitted with Circumferential Grooves and Varied Rotor Stator Darji A., Alone D. , Mistry C. S. By ASME GT India 2017 1-10 (2017)
• Criteria for selection of solidity in design of contra rotating fan stage Mistry C. S., Nayak N. By National Aerospace Propulsion Conference (NAPC) 1-10 (2017)
• Design aspects of large diameter, low speed axial flow fan for wind tunnel application Mistry C. S., Kesharwani S. , Roy S. , Roy A. , Sinhamahapatra K. P. By ASME GT India 1-10 (2017)
Book
• Proceedings of the National Aerospace Propulsion Conference Mistry C. S., Kishore Kumar S. , B. N. Raghunandan B. N., Gullapalli Sivaramakrishna G. By 1-546 (2020)
Workshop
• Numerical Studies To Understand an Effect OF Rotor-Stator Axial Gap On the Performance of Transonic Axial Flow Compressor Stage Coupled With Circumferential Grooved Casing Treatment Mistry C. S., Darji A. P., Alone D. B. By Asian Congress on Gas Turbines-2016 1-10 (2016)
• Performance Characterizations of a High Speed Axial Flow Compressor Stage Implemented With Diverse Porosities of Axial Slotted Casing Treatment Mistry C. S., Joseph J. S., Alone D. B. By Asian Congress on Gas Turbines-2016 1-10 (2016)
• Development Of Bell Mouth for Low Speed Axial Flow Compressor Testing Facility Mistry C. S., Tiwari A. , Patel S. , Lad A. By Asian Congress on Gas Turbines-2016 01-10 (2016)
• Investigations on the Effect of Inflow Distortion on the Performance of a High Aspect Ratio, Low Speed Contra-rotating Fan Stage Mistry, C.S. and Pradeep, A.M. By GT2013-94311, Proceedings of 2013 ASME TURBO EXPO, San Antonio, Texas, USA. 1-10 (2013)
• Study of the Velocity Flow Field Under Distorted Inflow Conditions for a High Aspect ratio Low Speed Contra Rotating Fan Mistry, C.S. and Pradeep, A.M. By GTIndia2013-3594, Proceedings of the 2013 ASME GT India Conference, Bangalore. 1-10 (2013)
• Effect of Speed Ratio and Axial Spacing Variations on the Performance of A High Aspect Ratio, Low Speed Contra-Rotating Fan Mistry, C.S. and Pradeep, A.M. By Proceedings of 2012 ASME TURBO EXPO, Copenhagen, Denmark. 1-10 (2012)
• Understanding The Flow Behavior In A Low Hub-Tip Ratio, High Aspect Ratio Contra-Rotating Axial Fan Stage Mistry, C.S. and Pradeep, A.M. By GTIndia2012-9531, Proceedings of the 2012 ASME GT India Conference, Mumbai. 1-10 (2012)
• Design and Performance Analysis of a Low-speed, High Aspect Ratio Contra-rotating Fan Stage Mistry, C.S. and Pradeep, A.M., By Proceedings of the 11th Asian International Conference on Fluid Machinery, IIT Madras. 1-10 (2011)
• Preliminary Design Concepts for High Solidity Nozzle-less Radial Inflow Gas Turbine for Small Capacity Gas Turbine Engine Mistry, C.S. and Channiwala, S.A. By GT2006-90962, Proceedings of 2006 ASME TURBO EXPO, Barcelona, Spain. 1-10 (2006)
• Comparative assessment on performance of multi-cylinder engine using CNG/LPG and petrol as a fuel Mistry, C.S. By 2005-01-1056, SAE 2005 World Congress & Exhibition, Detroit, USA 1-6 (2005)
• Performance Assessment of Multi-Cylinder Engine Using CNG Mistry, C.S., Gohil, P.P. and Sharma, D.M. By IMECE2005-79950, Proceedings of IMECE2005, USA. 1-6 (2005)
• Design of nozzle-less radial inflow gas turbine for small capacity(20kW) gas turbine engine Mistry, C.S. and Channiwala, S.A. By IMECE2004-59949, Proceedings of IMECE 2004,USA 1-10 (2004)
• Experimental Investigation On Multi-cylinder Engine Using Petrol and LPG as A Fuel Mistry, C.S. and Gandhi, A.H. By 2004-01-1653, SAE 2004 World Congress &Exhibition, Detroit, USA 1-6 (2004)

Principal Investigator

• Airavat- The Future of Transportation (ICG_2017)
• Experimental Investigations on Performance of Tandem Bladed Low Speed Axial Flow Compressor
• Contra-Rotating Axial-Centrifugal Compressor Stage Aerodynamics - An Experimental Investigation

Co-Principal Investigator

• Aerodynamic design of traction rolling stock with speed potentials of 250 km/h upgradeable up to 350 km/h
• Computational Flow Analysis and Simulation of Smoke and Particle Dispensation System through GAS Turbine System