Indian Institute of Technology Kharagpur |

Book Chapter/Section

Aerodynamic Design of Fan Rotors for Ultra-High-By-Pass-Ratio Turbofan Engines by Ernesto B., Mistry C. S. 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 by Bhavsar H., Mistry C. S. Proceedings of the National Aerospace Propulsion Conference 1-12 (2022)

Patent

Axial-centrifugal contra-rotating light weight, compact compression system by Mistry C. S., A. - (Accepted/In-Press)
AXIAL-CENTRIFUGAL CONTRA-ROTATING LIGHT WEIGHT, COMPACT COMPRESSION SYSTEM. by Mistry C. S., A. - (Accepted/In-Press)
Axial-centrifugal contra-rotating compressor system adapted for high thrust to weight ratio of gas turbine engine by Mistry C. S., A. - (2025)
AXIAL-CENTRIFUGAL CONTRA-ROTATING COMPRESSOR SYSTEM ADAPTED FOR HIGH THRUST TO WEIGHT RATIO OF GAS TURBINE ENGINE by Mistry C. S., A. - (2020)

Others

NPTEL COURSE : AEROENGINE GAS TURBINE CYCLES by Mistry C. S. - (2026)
NPTEL COURSE: AERODYNAMIC DESIGN OF AXIAL FLOW COMPRESSORS AND FANS by Mistry C. S. - (2025)

Journal

Thermodynamic and chemical kinetic analysis of a gas turbine power plant using hydrogen from onsite ammonia cracking for low-emission power generation by Pavan Kumar M.G., Sorrentino G., de Joannon M., Mistry C.S., Reddy V.M. Energy Conversion and Management 352 - (2026)
Thermodynamic and chemical kinetic analysis of a gas turbine power plant using hydrogen from onsite ammonia cracking for low-emission power generation by Maganti G. P., Joannon M. D., Sorrentino G. , Mistry C. S., Vanteru M. R. Energy Conversion and Management 352 121116- (2026)
Multirow sweeping jet film cooling on HP turbine vane leading edge with staggered arrangement by Sharma H., Roy A., Mistry C.S. Applied Thermal Engineering 289 - (2026)
Multirow sweeping jet film cooling on HP turbine vane leading edge with staggered arrangement. by Mistry C. S., Sharma H. , Roy A. Applied Thermal Engineering Volume 289, Part 2 - (2026)
Effect of Blowing Configurations on Heat Transfer Augmentation With Multihole Sweeping Jet Film Cooling by Sharma H., Pavan Kumar K.S., Roy A., Mistry C.S. ASME Journal of Heat and Mass Transfer 148 - (2026)
Sweeping Jet Film Cooling Over The Suction Surface of Hp Turbine NGV With Forward and Reversed Hole Configurations by Mistry C. S., Sharma H. , Roy A. Journal of Thermal Science and Engineering Applications 18(8) 1-14 (2026)
Sweeping Jet Film Cooling Over the Suction Surface of HP Turbine Nozzle Guide Vane With Forward and Reversed Hole Configurations by Sharma H., Mistry C.S., Roy A. Journal of Thermal Science and Engineering Applications 18 - (2026)
Numerical study on impact of circular pivot sizes on part clearance flow structure and loss mechanism within variable area low pressure turbine nozzle vanes by Bhavsar H., Mistry C. Aerospace Science and Technology 165 - (2025)
Study of Tandem Rotor Dual Wake Interaction with Downstream Stator under Unsteady Numerical Approach by Singh A., Mistry C. Journal of Engineering for Gas Turbines and Power 147 - (2025)
Detailed Flow Analysis of a Feedback channel type Fluidic Oscillator using Dynamic Mode Decomposition by Sharma H., Roy A. , Mistry C. S. AIAA Journal 1-19 (2025)
Detailed Flow Analysis of Feedback-Channel-Type Fluidic Oscillator Using Dynamic Mode Decomposition by Sharma H., Roy A., Mistry C.S. AIAA Journal 63 3231-3249 (2025)
Implementation of flow control methods for design of connecting duct of annular sector cascade tunnel by Bhavsar H., Mistry C. S. Journal of Engineering for Gas Turbines and Power 147(8) 081017-081031 (2025)
Investigations on Design Space for Highly Loaded Tandem Bladed Axial Flow Rotor- novel Stator for Low-speed Compressor Research Facility by Singh A., Mistry C.S. Journal of Applied Fluid Mechanics 17 2245-2265 (2024)
Characteristics of Laminar Separation Bubble With Varying Leading-Edge Shapes and Deflections of the Trailing-Edge Flap by Sarvankar S.S., Sarkar D., Arasu A.I., Mistry C.S., Vadlamani N.R. Journal of Engineering for Gas Turbines and Power 146 - (2024)
Characteristics of Laminar Separation Bubble With Varying Leading-Edge Shapes and Deflections of the Trailing-Edge Flap by , Sarvankar S. , Sarkar D. , Arasu A. , Mistry C. S., Rao N. Journal of Engineering for Gas Turbines and Power 146 - (2024)
Characterization of Leading-edge Laminar Separation Bubble for various Angles of Incidence and Reynolds Numbers by Bandopadhyay T., Mistry C.S. Journal of The Institution of Engineers (India): Series C 105 891-910 (2024)
Study on Part Clearance Flow Field for Variable Area LP Turbine Nozzle Vane using Different Turbulence Models by Bhavsar H., Mistry C. International Journal of Gas Turbine, Propulsion and Power Systems 15 108-117 (2024)
Study on Part Clearance Flow Field for Variable Area LP Turbine Nozzle Vane using Different Turbulence Models by , Bhavsar H. , Mistry C. S. International Journal of Gas Turbine, Propulsion and Power Systems - (2024)
Development of Curved Shape Diffuser-Duct for Aero-Engines With a Backend Centrifugal Compressor by Kumar A., Mistry C., Kumar S., Pratap A. Defence Science Journal 74 417-427 (2024)
Understanding of tip clearance flow structure in high speed mixed flow compressor by , Kumar H. , Mistry C. S. Propulsion and Power Research 12 356-379 (2023)
Understanding of tip clearance flow structure in high speed mixed flow compressor by H., Mistry C. S. Propulsion and Power Research 12(3) 356-379 (2023)
Effect of Axial Extension on Parameterized Endwall Contour with Incidence change for LP Turbine Linear Cascade by Darji A., Baloni B. , Mistry C. S. Journal of Mechanical Science and Technology 37 2223-2322 (2023)
Numerical Modelling of Wind Tunnel Internal Flow for CFD Assisted Design by Kesharwani S., Mistry C. S., Roy S. , Roy A. , Sinhamahapatra K. P. Journal of Institution of Engineers (India) Series C - (2022)
Effects of total pressure distribution on performance of small size counter-rotating Axial-flow fan stage for electrical propulsion by Mistry C. S., Bandopadhyay T. ASME Open Journal of Engineering 1-14 (2022)
Characterization of leading-edge laminar separation bubble for various angle of incidences and Reynolds numbers by Mistry C. S., Bandopadhyay T. Journal of The Institution of Engineers (India): Series C. , Springer 1-20 (2022)
Innovative Approach for Design and Development of Annular Sector Cascade Tunnel Using Numerical Analysis by Mistry C. S., Bhavsar H. Journal of The Institution of Engineers (India): Series C 1-21 (2021)
Structure and Vibration Analyses of Low Speed Contra-Rotating Fan Stage with High Aspect Ratio by Mistry C. S., Ghosh A. , Sah S. International Journal of Aerospace System Engineering 8 1-13 (2021)
Structure and Vibration Analyses of Low Speed Contra-Rotating Fan Stage with High Aspect Ratio by Mistry C. S., Ghosh A. , Sah S. International Journal of Aerospace System Engineering 1-10 (2021)
Propagation of Different Types of Inflow Distortions through a Contra Rotating Fan Stage by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M., 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 by Mistry, C.S. SAE2005 Transactions Journal of Passenger Cars-Electronic & Electrical systems March-2006 1-6 (2005)

Conferences

CYCLE ANALYSIS OF FUTURISTIC RDE-BASED SMALL TURBOJET AND TURBOPROP ENGINES FOR UAVS by Vigneswaran S., Ghosh A., Mistry C.S. ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) 4 - (2025)
SECONDARY FLOW LOSSES MITIGATION FOR LOW-PRESSURE TURBINE CASCADE USING RESPONSE SURFACE OPTIMIZATION by Darji A.P., Baloni B.D., Mistry C.S. Proceedings of the ASME Turbo Expo 10 - (2025)
Numerical Investigations on the Influence of Inflow Parameters on Secondary Flow for HP Turbine Nozzle Vane by Thuniki Shrenith Suhas ., Mistry C. S., Sinhamahapatra K. P. NAPC - 2025 1-14 (2025)
Impact of pivot geometry shapes and locations on variable stator vane compressor cascade by Salunkhe M., Mistry C. S. NAPC - 2025 1-14 (2025)
IMPACT OF SWEEPING JET INCLINATION ANGLES ON FILM COOLING PERFORMANCE ON HIGH-PRESSURE TURBINE NOZZLE GUIDE VANES by Kumar B.R., Sharma H., Roy A., Mistry C.S. ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) 4 - (2025)
EFFECT OF BLOWING CONFIGURATIONS ON HEAT TRANSFER AUGMENTATION WITH MULTIHOLE SWEEPING JET FILM COOLING by Sharma H., Pavan Kumar K.S., Roy A., Mistry C.S. Proceedings of the ASME Turbo Expo 5 - (2025)
EFFECT OF INFLOW TURBULENCE ON HEAT TRANSFER AUGMENTATION WITH MULTIHOLE SWEEPING JET FILM COOLING by Pavan Kumar K.S., Sharma H., Roy A., Mistry C.S. Proceedings of the ASME Turbo Expo 5 - (2025)
THE EFFECT OF CLEARANCE FLOW ON VARIABLE AREA NOZZLE VANE by Bhavsar H., Mistry C.S. ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) 4 - (2025)
ENHANCING FILM COOLING PERFORMANCE IN GAS TURBINES: THE IMPACT OF SWEEPING JETS AND ROW SPACING by Patel J., Sharma H., Roy A., Mistry C.S. ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) 4 - (2025)
Historical retrospective on technology advances in military aeroengines by Mistry C. S., Benini E. , Wadia A. ISABE 2024 1-15 (2024)
Numerical investigations on delay in onset of inflection for S-shaped compressor airfoil flow characteristics by S., Mistry C. S. Asian congress on Gas turbine 2024 1-10 (2024)
Optimization of high-speed LP Turbine blade profile using CAD-based parametrization and meta-modeling algorithms by Durvasula Bhaskara Rama Sarma ., Mistry C. S. ASIAN CONGRESS ON GAS TURBINES 2024 1-10 (2024)
SWEEPING JET FILM COOLING OVER THE SUCTION SURFACE OF HP TURBINE NGV WITH FORWARD AND REVERSED HOLE CONFIGURATIONS by Sharma H., Mistry C.S., Roy A. Proceedings of the ASME Turbo Expo 7 1-16 (2024)
INVESTIGATIONS ON UNSTEADY FLOW STRUCTURE FORMATION IN TANDEM BLADED AXIAL FLOW COMPRESSOR STAGE by Singh A., Mistry C.S. Proceedings of the ASME Turbo Expo 12A 1-16 (2024)
Implementation of Flow Control Methods for Design of Connecting Duct of Annular Sector Cascade Tunnel by Mistry C. S., Bhavsar H. GT India Gas Turbine India Conference 1-10 (2023)
Implementation of Similarity Principle and Scaling Laws for Low-to-High Speed Mixed Flow Compressor by Mistry C. S., Kumar H. Turbo Expo 2023 Turbomachinery Technical Conference & Exposition 1-14 (2023)
Innovative lightweight compression system based on axial-centrifugal contra-rotating concept: pushing the limits by Mistry C. S., A. , S. , Pratap A. Turbo Expo 2023 Turbomachinery Technical Conference & Exposition 1-15 (2023)
Characteristics of Laminar Separation Bubble with Varying Leading-Edge Shapes and Deflections of the Trailing-Edge Flap by Sarvankar S., Sarkar D. , Mistry C. S., Rao N. GT India Gas Turbine India Conference 1-11 (2023)
Computational Investigations of Effect of Reynolds Number on Secondary Losses and Flow Behavior in Linear Turbine Cascade by Mistry C. S., Darji A. P., Baloni B. D. GT India Gas Turbine India Conference 1-15 (2023)
Aerodynamic Design Aspects for Small-Size Transonic Contra-Rotating Fan Stage by Pasupula M., Mistry C. S. GT India Gas Turbine India Conference 1-12 (2023)
Secondary Losses Mitigation Using End Wall Contouring for LPT Nozzle Vane Cascade by S., Mistry C. S. GT India Gas Turbine India Conference 1-14 (2023)
Non-Axisymmetric Stator Hub Endwall Contouring for Tandem Bladed Axial Compressor Stage by S. P., Mistry C. S., Roy A. GT India Gas Turbine India Conference 1-15 (2023)
Strategic Design Approach for Future Fuselage BLI Engine Based Hybrid Propulsion System by Kolhe S., Bharade A. , Raj H. , Anantwar J. , Agrawal A. , Mandal G. , Mistry C. S. GT India Gas Turbine India Conference 1-8 (2023)
Study of Tandem Rotor Dual Wake Interaction With Downstream Stator Under Unsteady Numerical Approach by Singh A., Mistry C. S. GT India Gas Turbine India Conference 1-14 (2023)
Study on Part Clearance Flow Field for Variable Area LP Turbine Nozzle Vane using Different Turbulence Models by Bhavsar H., Mistry C. S. International Gas Turbine Congress 2023 1-15 (2023)
Study on secondary flow phenomena with variable leading edge fillet and endwall contouring on the low-pressure turbine vane linear cascade by , Darji A. , Baloni B. D., Mistry C. S. Turbo Expo 2023 Turbomachinery Technical Conference & Exposition 1-14 (2023)
Historical developments in fan technologies for Aeroengines by Mistry C. S., Benini E. , Wadia A. Turbo Expo 2023 Turbomachinery Technical Conference & Exposition 1-14 (2023)
Effect of Pivot-Shape Modifications on Part Clearance Flow Field in Variable Area Turbine Nozzle Vane by Mistry C. S., Mandal G. , Bhavsar H. GT India Gas Turbine India Conference 1-15 (2023)
Effect of Axial Extension on Parameterized Endwall Contour with Incidence change for LP Turbine Linear Cascade by Darji A., Baloni B. D., Mistry C. S. Asian Congress on Gas Turbines 2022 (ACGT2022) 1-12 (2022)
Effects of head geometry on five-hole pressure probes for wide angular range by Singh A., J. , Mistry C. S. 4th National Aerospace Propulsion Conference (NAPC-2022) 1-10 (2022)
Parametric study of DCA airfoil using MISES by Mandal G., Mistry C. S. 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 by Bhavsar H., Mistry C. S. 4th National Aerospace Propulsion Conference (NAPC-2022) 1-14 (2022)
Passive flow control approach for design of wide angle diffuser of linear cascade tunnel by Bhavsar H., Mistry C. S. 4th National Aerospace Propulsion Conference (NAPC-2022) 1-12 (2022)
Development of Curved Shape Diffuser-Duct for Aero-Engines with a Backend Centrifugal Compressor by A., Mistry C. S., S. , Pratap A. 4th National Aerospace Propulsion Conference (NAPC-2022) 1-14 (2022)
Development of time-efficient multi-hole pressure probe calibration facility by Singh A., Kumar A., Tayal G., Mistry C. Lecture Notes in Mechanical Engineering 313-336 (2021)
Numerical investigations on aerodynamic design criteria for low speed mixed flow compressor by Kumar H., Mistry C.S. 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 by Tanwar B.P.S., Singh A., Mistry C.S. 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 by Darji A.P., Baloni B.D., Mistry C.S. Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021 - (2021)
Extending the angular measurement range of a miniature 5-hole probe for measurements in turbomachines by Singh A., A. , Bhavsar H. , Mistry C. S. AeSI International Conference 1-10 (2020)
Flow Study of Tandem Arrangement of Intakes at Take-off Condition for an Electrical Vehicle by Mistry C. S., Sai Subhankar V. , A. , Surampally V. , Rathi D. , Bandopadhyay T. National Aerospace Propulsion Conference (NAPC) 1-12 (2020)
High Speed Turbo Pump Inducer Sensitive Response of Cavitating Flow, its Modulation and Challenges by Mistry C. S., Akula P. National Aerospace Propulsion Conference (NAPC) 1-7 (2020)
Aerodynamic design aspects for stator of highly loaded tandem bladed axial compressor by Singh A., Mistry C.S. Proceedings of the ASME Turbo Expo 2A-2020 - (2020)
Effect of Various Periodic Surface Concepts for Numerical Investigation of Flow Field Through Variable Area LP Turbine Nozzle by Mistry C. S., Bhavsar H. National Aerospace Propulsion Conference (NAPC) 1-10 (2020)
Numerical Analysis on Effect of Tip Clearance Flow for LP Turbine Linear Cascade by Gedam A., M. , Bhavsar H. , Mistry C. S. 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 by Bhavsar H., Mistry C. S. ASME Turbo Expo-2020 1-10 (2020)
Numerical performance and flow field study of centrifugal compressor with supercritical carbon-dioxide (SCO2) by Kumar H., Mistry C.S. 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 by Bhavsar H., Mistry C.S. ASME 2019 Gas Turbine India Conference, GTINDIA 2019 1 - (2019)
Effects of total pressure distribution on performance of small size counter-rotating axial-flow fan stage for electrical propulsion by Bandopadhyay T., Mistry C.S. 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 by Singh A., Mistry C.S. Proceedings of the ASME Turbo Expo 2A-2019 - (2019)
Parametric study for adoption of variable cycle engine concept for low bypass ratio turbofan engine by Swaminathan K., Mistry C.S. ASME 2019 Gas Turbine India Conference, GTINDIA 2019 2 - (2019)
DEVELOPMENT OF TIME EFFICIENT MULTIHOLE PRESSURE PROBE CALIBRATION FACILITY by Singh A., A. , G. , Mistry C. S. National AErospace Propulsion Conference - (2018)
Structural and Vibration Analysis of High Aspect ratio Low Speed Contra-Rotating Fan Stage by Sah S. K., Ghosh A. , Mistry C. S. 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 by Darji A., Alone D. , Mistry C. S. ASME GT India 2017 1-10 (2017)
Criteria for selection of solidity in design of contra rotating fan stage by Mistry C. S., Nayak N. National Aerospace Propulsion Conference (NAPC) 1-10 (2017)
Design aspects of large diameter, low speed axial flow fan for wind tunnel application by Mistry C. S., Kesharwani S. , Roy S. , Roy A. , Sinhamahapatra K. P. ASME GT India 1-10 (2017)

Educational Package

Aerodynamic design of Axial Flow Compressors and Fans by Mistry C. S. - (2023)
AeroEngine Gas Turbine Cycles by Mistry C. S. - (2023)
Aerodynamic Design of Axial Flow Compressors & Fans by Mistry C. S. - (2022)

Symposium

Particulate Laden Exhaust Gas Spread from Jet Engines by Prakash A., Mistry C. S., Garg A. , Vasistha P. 15th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows 1-10 (2023)
Simulation of Particulate Dusting by Prakash A., Mistry C. S., Garg A. , Vasistha . 15th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows 1-8 (2023)

Edited Volume

Recent Advances in Computational and Experimental Mechanics, Vol I by Maity D., Patra P. K., Afzal M. S., Ghoshal R. , Mistry C. S., Jana P. , Maiti D. K. Recent Advances in Computational and Experimental Mechanics, Vol I - (2022)
Recent Advances in Computational and Experimental Mechanics, Vol II by Maiti D. K., Jana P. , Mistry C. S., Ghoshal R. , Afzal M. S., Patra P. K., Maity D. Recent Advances in Computational and Experimental Mechanics, Vol II - (2022)

Book

Proceedings of the National Aerospace Propulsion Conference by Mistry C. S., Kishore Kumar S. , B. N. Raghunandan B. N., Gullapalli Sivaramakrishna G. 1-546 (2020)

Workshop

Performance Characterizations of a High Speed Axial Flow Compressor Stage Implemented With Diverse Porosities of Axial Slotted Casing Treatment by Mistry C. S., Joseph J. S., Alone D. B. Asian Congress on Gas Turbines-2016 1-10 (2016)
Development Of Bell Mouth for Low Speed Axial Flow Compressor Testing Facility by Mistry C. S., Tiwari A. , Patel S. , Lad A. Asian Congress on Gas Turbines-2016 01-10 (2016)
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 by Mistry C. S., Darji A. P., Alone D. B. Asian Congress on Gas Turbines-2016 1-10 (2016)

Investigations on the Effect of Inflow Distortion on the Performance of a High Aspect Ratio, Low Speed Contra-rotating Fan Stage by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M. 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 by Mistry, C.S. and Pradeep, A.M., 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 by Mistry, C.S. and Channiwala, S.A. 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 by Mistry, C.S. 2005-01-1056, SAE 2005 World Congress & Exhibition, Detroit, USA 1-6 (2005)
Performance Assessment of Multi-Cylinder Engine Using CNG by Mistry, C.S., Gohil, P.P. and Sharma, D.M. IMECE2005-79950, Proceedings of IMECE2005, USA. 1-6 (2005)
Design of nozzle-less radial inflow gas turbine for small capacity(20kW) gas turbine engine by Mistry, C.S. and Channiwala, S.A. IMECE2004-59949, Proceedings of IMECE 2004,USA 1-10 (2004)
Experimental Investigation On Multi-cylinder Engine Using Petrol and LPG as A Fuel by Mistry, C.S. and Gandhi, A.H. 2004-01-1653, SAE 2004 World Congress &Exhibition, Detroit, USA 1-6 (2004)

Aerospace Engineering

Faculty

Chetankumar Sureshbhai Mistry

Research Areas

Principal Investigator

Ph. D. Students

Akchhay Kumar

Hitesh Sharma

Praveen Kumar Akula

Vibhash Hembram