Prof. Chetankumar Mistry

Book

1. Proceedings of the National Aerospace Propulsion Conference , Editors: Mistry, C.S., Kumar, S.K., Raghunandan, B.N., Sivaramakrishna, G. (Eds.), 2020 Springer Nature Switzerland AG. Part of Springer Nature.

2. Recent Advances in Computational and Experimental Mechanics, Select Proceedings of ICRACEM 2020 Vol I, Editors: Maity, D., Patra, P.K., Afzal, M.S., Ghoshal, R., Mistry, C.S., Jana, P., Maiti, D.K. (Eds.), 2022 Springer Singapore . Part of Springer Nature.

3. Recent Advances in Computational and Experimental Mechanics, Select Proceedings of ICRACEM 2020 Vol II, Editors: Maiti, D.K., Jana, P., Mistry, C.S., Ghoshal, R., Afzal, M.S., Patra, P.K., Maity, D. (Eds.), 2022 Springer Singapore . Part of Springer Nature.

Book Chapter

Ajey Singh, Akchhaykumar, Gaurav Tayal, Chetan Mistry, 2020,“Development of time efficient multihole pressure probe calibration facility”, In book: Proceedings of the National Aerospace Propulsion Conference, Springer Nature Switzerland AG. Part of Springer Nature.

Bhavsar,H., Mistry, C.S., 2022, "Effect of Various Periodic Surface Concepts for Numerical Investigation of Flow Field Through Variable Area LP Turbine Nozzle" In book: Proceedings of the National Aerospace Propulsion Conference, Springer Nature Switzerland AG. Part of Springer Nature.

Ernesto Benini, Chetan S. Mistry,2023 "Aerodynamic Design of Fan Rotors for Ultra-High-By-Pass-Ratio Turbofan Engines" AIAA educational series book.

In communication:

1. Ajey Singh, Chetan Mistry,2026,“Effect of rotor-stator axial gap on the performance of tandem bladed axial flow compressor "In communication

2. DSBR Sarma, Hardikkumar Bhavsar, Chetan S. Mistry,2026 "Effect of Probe Head Geometry and Mach Number on Five-Hole Pressure Probe Calibration for Turbine Cascade Applications," in communication

3. Sharma, H., and Roy, A.Mistry, C. S., (2026) Experimental Investigation of Sweeping Jet Film Cooling over the Leading Edge of HP Turbine Vane: Effect of Freestream Reynolds Number at Density Ratio of 0.8.

4. Saha. P,Halder,S., Das., D, Mistry,C.S., Three Dimensional Shock Boundary Layer Interaction Governing Unstart in Supersonic Guide Vanes.

Journal Articles

1. MGP Kumar, G Sorrentino, M de Joannon, CS Mistry, VM Reddy, (2026), “Multirow sweeping jet film cooling on HP turbine vane leading edge with staggered arrangement.” Energy Convers. Manag. March 2026; 352: 121116. https://doi.org/10.1016/j.enconman.2026.121116

2. Sharma, H., Roy, A.and Mistry, C. S., (2026). "Sweeping Jet Film Cooling Over The Suction Surface of Hp Turbine NGV With Forward and Reversed Hole Configurations." ASME. J. Thermal Sci. Eng. Appl. doi: https://doi.org/10.1115/1.4070975

3. Sharma, H., Roy, A., Mistry, C. S., (2026), “Multirow sweeping jet film cooling on HP turbine vane leading edge with staggered arrangement.” Appl. Therm. Eng. March 2026; 289 (2): 129736. https://doi.org/10.1016/j.applthermaleng.2026.129736

4. Sharma, H., Pavan Kumar, K. S., Roy, A., and Mistry, C. S., (2025), “Effect of Blowing Configurations on Heat Transfer Augmentation With Multihole Sweeping Jet Film Cooling.” ASME. J. Heat Mass Transfer. January 2026; 148(1): 012302. https://doi.org/10.1115/1.4069892

5. Bhavsar, H., Mistry, C., (2025), “Numerical study on impact of circular pivot sizes on part clearance flow structure and loss mechanism within variable area low pressure turbine nozzle vanes.” Aerosp. Sci. Technol. October 2025; 165: 110497. https://doi.org/10.1016/j.ast.2025.110497

6. Sharma, H., Roy, A., Mistry, C. S., (2025), “Detailed Flow Analysis of a Feedback channel type Fluidic Oscillator using Dynamic Mode Decomposition.” AIAA Journal 2025 63(8): 3231-3249. https://doi.org/10.2514/1.J064809

7. Bhavsar,H., Mistry, C.S., (2025), “Implementation of flow control methods for design of connecting duct of annular sector cascade tunnel.” J. Eng. Gas Turbines Power. Aug 2025, 147(8): 081017. https://doi.org/10.1115/1.4067707

8. Singh, A., and Mistry, C., (2024), “Study of Tandem Rotor Dual Wake Interaction With Downstream Stator Under Unsteady Numerical Approach.” ASME. J. Eng. Gas Turbines Power. August 2025; 147(8): 081007. https://doi.org/10.1115/1.4067094

9. Kumar, A., Mistry, C., Kumar, S., & Pratap, A., (2024), “Development of Curved Shape Diffuser Duct for Aero Engines With a Backend Centrifugal Compressor.” Defence Science Journal, 74(4), 417–427. https://doi.org/10.14429/dsj.74.20030

10. Bhavsar, H., and Mistry, C., (2024), “Study on Part Clearance Flow-field for Variable Area LP Turbine Nozzle Vane Using Different Turbulence Models.” Int. J. Gas Turbine, Propuls. Power Syst., 15(3), pp. 108–117. https://doi.org/10.38036/jgpp.15.3_114

11. Sarvankar, S. S., Sarkar, D., Arasu, A. I., Mistry, C. S., and Vadlamani, N. R., (2024). “Characteristics of Laminar Separation Bubble With Varying Leading-Edge Shapes and Deflections of the Trailing-Edge Flap.” ASME. J. Eng. Gas Turbines Power. October 2024; 146(10): 101014. https://doi.org/10.1115/1.4065408

12. Ajey Singh, Mistry, C.S., (2024), “Investigations On Design Space for Highly Loaded Tandem Bladed Axial Flow Rotor- Novel Stator for Low-Speed Research Facility.” J. Appl. Fluid Mech., January-2024 17(10): 90. https://doi.org/10.47176/jafm.17.10.2521

13. Hemantkumar, Mistry, C.S., (2023), "Understanding of tip clearance flow structure in high-speed mixed flow compressor.” J. Propul. Power Res., September 2023; 12(3), 356-379.

14. Darji, A.P., Baloni, B.D. & Mistry, C.S., (2023), “Effect of axial extension on parameterized endwall contour with incidence change for low-pressure turbine linear cascade.” J Mech Sci Technol 37, 2223–2232 (2023). https://doi.org/10.1007/s12206- 023-2109-7

15. Darji, A. P., Baloni, B. D., and Mistry, C. S., (2022), “Numerical Investigations on Effect of Inflow Parameters on Development of Secondary Flow Field for Linear Low-Pressure Turbine Cascade.” ASME. J. Turbomach. May 2023; 145(5): 051008. https://doi.org/10.1115/1.4056093

16. Bandopadhyay, T., Mistry, C.S., (2022), “Characterization of Leading-edge Laminar Separation Bubble for various Angles of Incidence and Reynolds Numbers.” J. Inst. Eng. India Ser. C 105, 891–910 (2024). https://doi.org/10.1007/s40032-022-00831-x

17. Bandopadhyay, T., and Mistry, C. S., “Effects of Total Pressure Distribution on Performance of Small-Size Counter-Rotating Axial-Flow Fan Stage for Electrical Propulsion.” ASME Open J. Engineering ASME. January 2022 1 011012 doi: https://doi.org/10.1115/1.4053962

18. Numerical Modelling of Wind Tunnel Internal Flow for CFD Assisted Design.” J. Inst. Eng. India Ser. C 105, 839–859 (2024). https://doi.org/10.1007/s40032-021- 00794-5

19. Bhavsar, H., Mistry, C.S., (2021), “Innovative Approach for Design and Development of Annular Sector Cascade Tunnel using Numerical Analysis.” J. Inst. Eng. India Ser. C 105, 861–876 (2024). https://doi.org/10.1007/s40032-021-00770-z

20. Sah, S.K., Ghosh, A., Mistry, C.S., (2021), “Structure and Vibration Analyses of Low Speed Contra-Rotating Fan Stage with High Aspect Ratio.” International Journal of Aerospace System Engineering, 2021; 8(1). https://doi.org/10.20910/IJASE.2021.8.1.1

21. Mistry, C.S. and Pradeep, A.M., (2014), “Experimental Investigation of a High Aspect Ratio, Low Speed Contra Rotating Fan Stage with Complex Inflow Distortion.” Propuls. Power Res. June, 2014, 3(2), pp. 68-81. https://doi.org/10.1016/j.jppr.2014.05.005

22. Mistry, Chetan and Pradeep, A.M., (2014), “Propagation of Different Types of Inflow Distortions through a Contra Rotating Fan Stage.” International Journal of Turbo & Jet-Engines, 2015; 32(1), pp. 41-57. https://doi.org/10.1515/tjj-2014-

23. Mistry, Chetan, Pradeep, A. M., (2014), “Experimental Study of the Effect of Radially Distorted Inflow on a Contrarotating Fan Stage.” International Journal of Rotating Machinery, 2014, 503579, 14 pages, 2014. https://doi.org/10.1155/2014/503579

24.Distortion on the Performance of a Low Speed, High Aspect Ratio Contra Rotating Axial Fan.” ASME. J. Turbomach. July 2014; 136(7): 071009. https://doi.org/10.1115/1.4025953

25. Mistry C, Pradeep A., (2013), “Effect of variation in axial spacing and rotor speed combinations on the performance of a high aspect ratio contra-rotating axial fan stage.” Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 2013;227(2):138-146. https://doi.org/10.1177/0957650912467453

26. Mistry, C. S., (2005), “Comparative Assessment on Performance of Multi cylinder Engine Using CNG, LPG and Petrol as a Fuel.” SAE Transactions, JOURNAL OF PASSENGER CARS: ELECTRONIC AND ELECTRICAL SYSTEMS (2005) 114 (7), 222–226. http://www.jstor.org/stable/44682422

Conference Articles

1. Mistry, C.S. and Channiwala, S.A.,2004 “ Design of nozzle-less radial inflow gas turbine for small capacity(20kW) gas turbine engine”, IMECE2004-59949, Proceedings of IMECE 2004,USA.

2. Mistry, C.S. and Gandhi, A.H., 2004, “Experimental Investigation On Multi-cylinder Engine Using Petrol and LPG as A Fuel”, 2004-01-1653, SAE 2004 World Congress &Exhibition, Detroit, USA.

3. Mistry, C.S., Gohil, P.P. and Sharma, D.M., 2005, “Performance Assessment of Multi-Cylinder Engine Using CNG”, IMECE2005-79950, Proceedings of IMECE2005, USA.

4. Mistry, C.S., 2005 “Comparative assessment on performance of multi-cylinder engine using CNG/LPG and petrol as a fuel”, 2005-01-1056, SAE 2005 World Congress & Exhibition, Detroit, USA.

5. Mistry, C.S. and Channiwala, S.A., 2006, “Preliminary Design Concepts for High Solidity Nozzle-less Radial Inflow Gas Turbine for Small Capacity Gas Turbine Engine”, GT2006-90962, Proceedings of 2006 ASME TURBO EXPO, Barcelona, Spain.

6. Mistry, C.S. and Pradeep, A.M., 2011, “Design and Performance Analysis of a Low-speed, High Aspect Ratio Contra-rotating Fan Stage”, Proceedings of the 11th Asian International Conference on Fluid Machinery, IIT Madras.

7. Mistry, C.S. and Pradeep, A.M., 2012, “Effect of Speed Ratio and Axial Spacing Variations on the Performance of A High Aspect Ratio, Low Speed Contra-Rotating Fan”, GT2012-68383, Proceedings of 2012 ASME TURBO EXPO, Copenhagen, Denmark.

8. Mistry, C.S. and Pradeep, A.M., 2012, “Understanding The Flow Behavior In A Low Hub-Tip Ratio, High Aspect Ratio Contra-Rotating Axial Fan Stage”, GTIndia2012-9531, Proceedings of the 2012 ASME GT India Conference, Mumbai.

9. Mistry, C.S. and Pradeep, A.M., 2013, “Investigations on the Effect of Inflow Distortion on the Performance of a High Aspect Ratio, Low Speed Contra-rotating Fan Stage”, GT2013-94311, Proceedings of 2013 ASME TURBO EXPO, San Antonio, Texas, USA.

10. Mistry, C.S. and Pradeep, A.M., 2013, “Study of the Velocity Flow Field Under Distorted Inflow Conditions for a High Aspect ratio Low Speed Contra Rotating Fan”, GTIndia2013-3594, Proceedings of the 2013 ASME GT India Conference, Bangalore.

11. Apurva Tiwari, Sahil Patel, Arpit Lad and Mistry, C.S.,2016 "Development Of Bell Mouth for Low Speed Axial Flow Compressor Testing Facility", ACGT2016-18, Proceedings of the Asian Congress on Gas Turbines, Bombay.

12. Anand P. Darji,Dilipkumar Bhanudasji Alone and Mistry, C.S., 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"ACGT2016-06, Proceedings of the Asian Congress on Gas Turbines, Bombay.

13. Jeffrey Savio Joseph, Dilipkumar Bhanudasji Alone and Mistry, C.S., 2016, "Performance Characterization of a High Speed Axial Flow Compressor Stage Implemented WITH Diverse Porosities OF Axial Slotting Casing Treatment"ACGT2016-02, Proceedings of the Asian Congress on Gas Turbines, Bombay.

14. Nayak ,N., Mistry, C.S., 2017, "Criteria for selection of solidity in design of contra rotating fan stage. "NAPC-2017, IIT Kanpur.

15. Darji,A.P., Alone, D.B. and Mistry, C.S., 2017, “ Flow Studies On a Single Stage Transonic Axial Flow Compressor Retrofitted with Circumferential Grooves and Varied Rotor Stator” GT India2016, Bangalore.v

16. Kesharwani,S., Mistry, C.S., Roy, S., Roy, R. and Mahapatra,K., 2017, “Design aspects of large diameter, low speed axial flow fan for wind tunnel application”, GT India2017, Bangalore.

17. Supen Sah, Anup Gosh, Chetan Mistry " Structural and Vibration Analysis of High Aspect ratio Low Speed Contra-Rotating Stage" ICTACEM 2017 , West Bengal.

18. Ajey Singh, Akchhaykumar, Gaurav Tayal, Chetan Mistry,“Development of time efficient multihole pressure probe calibration facility”,NAPC- 2018,IIT Kharagpur.

19. Ajey Singh, Chetan Mistry,“Study on effect of axial overlap on tip leakage flow structure in tandem bladed low speed axial flow compressor”ASME Turbo expo-2019, USA.

20. Bandopadhyay,T., Mistry, C.S., 2019, "Effects of total pressure distribution on performance of small size counter-rotating Axial-flow fan stage for electrical propulsion", GT India2019, Madras.

21. Bhavsar,H., Mistry, C.S., 2019, "Numerical study of part clearance and free stream turbulence on high end-wall LP Turbine nozzle annular cascade"”, GT India2019, Madras.

22. Hemantkumar., Mistry, C.S., 2019, "Numerical performance and flow field study of centrifugal compressor with Supercritical carbon-dioxide (SCO2)", GT India2019, Madras.

23. Swaminathan,K., Mistry, C.S., 2019, " Parametric study for adoption of Variable Cycle Engine concept for low bypass ratio Turbofan engine",GT India2019, Madras.

24. Ajey Singh, Akchhaykumar, Bhavsar,H., Mistry, C.S.,"Extending the angular measurement range of a miniature 5-hole probe for measurements in turbomachines"AeSI International Conference, March 6- 7, 2020, Kolkata.

25. Gedam, A. , Mohit Kumar, Bhavsar, H., Dr. Chetan S Mistry,2020, "Numerical Analysis on Effect of Tip Clearance Flow for LP Turbine Linear Cascade", AeSI International Conference, March 6- 7, 2020, Kolkata.

26. Ajey Singh, Chetan Mistry,2020,“Aerodynamic Design Aspects for Stator of Highly Loaded Tandem Bladed Axial Compressor " ASME Turbo expo-2020, London,UK.

27. Bhavsar,H., Mistry, C.S., 2020,"Numerical investigations on the effect of pivot shapes in part clearance flow field of variable area LP Turbine nozzle vane" ASME Turbo expo-2020, London,UK.

28. Bhavsar,H., Mistry, C.S., 2020, "Effect of Various Periodic Surface Concepts for Numerical Investigation of Flow Field Through Variable Area LP Turbine Nozzle", NAPC-2020, Bangalore.

29. Praveen Kumar Akula & Chetan S Mistry, “ High Speed Turbo Pump Inducer Sensitive Response of Cavitating Flow, its Modulation and Challenges”, NAPC-2020, Bangalore.

30. Varanasi Sai Subhankar, Amit Kumar, Venkatesh Surampally, Divvansh Rathi, Tuhin Bandopadhyay and Chetan S Mistry, “ Flow Study of Tandem Arrangement of Intakes at Take-off Condition for an Electrical Vehicle”, NAPC-2020, Bangalore.

31. Bhanu Pratap Singh Tanwar, Ajey Singh, Chetan Mistry,2021,“ Numerical Investigations on Application of Cantilever Stator on Aerodynamic performance of Tandem Bladed Axial-Flow Compressor " ASME Turbo expo-2021, Virtual.

32. Hemantkumar, Mistry, C.S., 2021, "Numerical Investigations on Aerodynamic Design Criteria for Low Speed Mixed Flow Compressor", GT India2021, Virtual.

33. Anand P. Darji, and Mistry, C.S., 2021, " Numerical investigations on effect of inflow parameters on development of secondary flow field for linear LP Turbine cascade", GT India2021, Virtual.

34. Anand P. Darji, Beena D. Baloni, and Mistry, C.S., "Effect of Axial Extension on Parameterized Endwall Contour with Incidence change for LP Turbine Linear Cascade", ACGT-2022.

35. Bhavsar,H., Mistry, C.S., 2022, "Parametric Study on Different Size of Circular Pivots in Part Clearance of Variable Area LP Turbine Nozzle Vane" NAPC-2022, IIT Bombay.

36. Bhavsar,H., Sarkar,S., Mistry, C.S., 2022, "Passive flow control approach for design of wide angle diffuser of linear cascade tunnel" NAPC-2022, IIT Bombay.

37. Mandal, G, Mistry, C.S., 2022, " Parametric study of DCA airfoil using MISES", NAPC-2022, IIT Bombay.

38. Ajey Singh, Jagdeeshwaran, J., , Bhavsar,H., Sarakar.D, Mistry, C.S., 2022, "Effects of head geometry on five-hole pressure probes for wide angular range", NAPC-2022, IIT Bombay.

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9. Akchhaykumar, Mistry, C.S.,Sankarkumar, Ajay Pratap, 2022,"Development of Curved Shape Diffuser-Duct for Aero-Engines with a Backend Centrifugal Compressor" NAPC-2022, IIT Bombay.

40. E. Benini, C. S. Mistry, A. R. Wadia, 2023,"Historical developments in fan technologies for Aeroengines", ASME Turbo expo-2023, USA.

41.Hemantkumar, Mistry, C.S., 2023," Implementation of Similarity Principle and Scaling Laws for Low-to-High Speed Mixed Flow Compressor. " ASME Turbo expo-2023, USA.

42. Anand P. Darji, Beena D. Baloni, and Mistry, C.S.,2023,"Study on secondary flow phenomena with variable leading edge fillet and endwall contouring on the low-pressure turbine vane linear cascade" ASME Turbo expo-2023, USA.

43. Akchhaykumar, Mistry, C.S., Sankarkumar, Ajay Pratap, 2023, "Innovative lightweight compression system based on axial-centrifugal contra-rotating concept: pushing the limits" ASME Turbo expo-2023, USA.

44. Prakash A., Mistry, C.S., Garg,A. , Vasistha. P, 2023, "Simulation of Particulate Dusting " 15th international symposium on experimental and computational aerothermodynamics of internal flows, IIT Madras, India.

45. Prakash A., Garg,A. , Vasistha.P, Mistry, C.S., 2023, "Particulate Laden Exhaust Gas Spread from Jet Engines " 15th international symposium on experimental and computational aerothermodynamics of internal flows, IIT Madras, India.

46. Anand P. Darji, Beena D. Baloni, and Mistry, C.S.,2023,"Computational Investigations of Effect of Reynolds Number on Secondary Losses and Flow Behavior in Linear Turbine Cascade " ASME GTIndia-2023,Bangalore,India.

47. Mandal., G, Bhavsar,H., Mistry, C.S., 2023, " Effect of Pivot-Shape Modifications on Part Clearance Flow Field in Variable Area Turbine Nozzle Vane" ASME GTIndia-2023, Bangalore, India.

48. Bhavsar,H., Mistry, C.S., 2023, " Implementation of Flow Control Methods for Design of Connecting Duct of Annular Sector Cascade Tunnel" Accepted for presentation ASME GTIndia-2023, Bangalore, India.

49. Shivkumar, Mistry, C.S., 2023, " Secondary Losses Mitigation Using End Wall Contouring for LPT Nozzle Vane Cascade" ASME GTIndia-2023, Bangalore, India.

50. Priyanka, Mistry, C.S., 2023, " Non-Axisymmetric Stator Hub Endwall Contouring for Tandem Bladed Axial Compressor Stage " ASME GTIndia-2023, Bangalore, India.

51. Ajey Singh, Chetan Mistry,2023,“Study of Tandem Rotor Dual Wake Interaction With Downstream Stator Under Unsteady Numerical Approach" ASME GTIndia-2023, Bangalore, India.

52. Surendra Kiran Kolhe, Aditya Bharade, Harsh Raj, Jay Anantwar, Abhishek Agrawal, Goutam Mandal, Mistry, C.S., 2023, "Strategic Design Approach for Future Fuselage Bli Engine Based Hybrid Propulsion System" ASME GTIndia-2023, Bangalore, India.

53. Manideep Pasupula, Mistry, C.S., 2023, "Aerodynamic Design Aspects for Small-Size Transonic Contra-Rotating Fan Stage" ASME GTIndia-2023, Bangalore, India.

54. Sumit Sarvankar , Drik Sarkar, Chetan Mistry,Rao,N. 2023, "Characteristics of Laminar Separation Bubble With Varying Leading-Edge Shapes and Deflections of the Trailing-Edge Flap" ASME GTIndia-2023, Bangalore, India.

55. Bhavsar,H., Mistry, C.S., 2023, "Study on Part Clearance Flow Field for Variable Area LP Turbine Nozzle Vane using Different Turbulence Models", International Gas Turbine Congress 2023,Kyoto, Japan.

56. E. Benini, C. S. Mistry, A. R. Wadia, 2023,"Historical retrospective on technology advances in military aeroengines ", Accepted for presentation in ISABE-2024.

56.Ajey Singh, Chetan Mistry,2024, “Investigations on unsteady flow structure formation in tandem Bladed axial flow compressor stage" TurboExpo-2024 , London.

57. Sharma, H., Mistry C.S, Roy A., "Sweeping jet film cooling over the suction surface of HP turbine NGV with forward and reversed hole configurations" TurboExpo-2024, London.

58. Shivakumar, Mistry, C.S., 2024,"Numerical investigations on delay in onset of inflection for S-shaped compressor airfoil flow characteristics", Asian Congress on Gas Turbine-2024, IIT Kanpur.

59. Durvasula Sai Bhaskara Rama Sarma,Mistry, C.S., 2024,"Optimization of high-speed LP Turbine blade profile using CAD-based parametrization and meta-modeling algorithms", Asian Congress on Gas Turbine-2024, IIT Kanpur.

60. E. Benini, C. S. Mistry, A. R. Wadia, 2023,"Historical retrospective on technology advances in military aeroengines ", ISABE-2024.

61. Suhas S.T., K. P Sinhamahapatra, Mistry, C.S., 2025," Numerical Investigations on the Influence of Inflow Parameters on Secondary Flow for HP Turbine Nozzle Vane" Accepted for presentation in NAPC-2025,IIT Madras.

62. Mandar. U.S, Mistry, C.S., 2025,"Impact of pivot geometry shapes and locations on variable stator vane compressor cascade" Accepted for presentation in NAPC-2025,IIT Madras.

63. Sharma, H., K S Pavan Kumar, Roy A., Mistry C.S, 2025"Effect of Blowing Configurations on Heat Transfer Augmentation With Multihole Sweeping Jet Film Cooling". TurboExpo-2025, USA

64. K S Pavan Kumar, Sharma, H., Roy A., Mistry C.S, 2025, "Effect of Inflow Turbulence on Heat Transfer Augmentation With Multihole Sweeping Jet Film Cooling" TurboExpo-2025, USA

65. Anand P. Darji, Beena D. Baloni, and Mistry, C.S.,2025, " Secondary flow losses mitigation for low-pressure turbine cascade using response surface optimization" TurboExpo-2025, USA

66. Bhavsar,H., Mistry, C.S., 2025, " The Effect of Clearance Flow on Variable Area Nozzle Vane", IMECE-2025 Hyderabad.

67.Bala Revath, Sharma, H., Roy A., Mistry C.S, 2025, Impact of Sweeping Jet Inclination Angles on Film Cooling Performance of High-Pressure Turbine Nozzle Guide Vanes", IMECE-2025 Hyderabad.

68. Jenish Patel, Sharma, H., Roy A., Mistry C.S, 2025, Enhancing Film Cooling Performance in Gas Turbines: The Impact of Sweeping Jets and Row Spacing.", IMECE-2025 Hyderabad.

69. Daksh Gupta D., Revanth Kumar B., Sharma, H., Roy A., Mistry C.S.,2026“ Aero-thermal investigations of sweeping jet film cooling on vki ls 89 cascade leading edge” TurboExpo-2026 (Paper under review)

70. Shrenith T.,Bhavsar H.,Sinhamahapatra K P., Mistry C.S.,2026, , “Numerical investigation of endwall purge cooling and secondary flow dynamics in high-pressure turbine nozzle guide vanes” TurboExpo-2026 (Paper under review)

71. Saha P.,Haldar S.,Das D., Mistry C.S.,2026, “Role of shock-boundary layer interaction in driving unstart phenomenon in supersonic turbine passages”TurboExpo-2026 (Paper under review)