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Dr. Gautam Choubey

Qualification : Ph.D.

D.O.J : 25-10-2018

Details of Educational Qualification:

Course Specialization Group College Name/University Year of Passing
Ph.D. Mechanical Engineering Mechanical Engineering National Institute of Technology, Silchar 2018
M.Tech. Thermal Engineering Mechanical Engineering National Institute of Technology Silchar 2014
B.Tech. Mechanical Engineering Mechanical Engineering I. K Gujral Punjab Technical University (A State Govt. University) 2012

Note : Students are advised to meet me in Room No : WB - 002 A at any time other than my class hours mentioned in the below timetable for any discussions related to the subjects & research.

My Schedule for 2019-20

                  

My Publications

S.No Title of the Paper Full Details of Journal Name / Conference Name, Volume number, page number, Date
1 Effect of variation of inlet boundary conditions on the combustion flow-field of a typical double cavity scramjet combustor International Journal of Hydrogen Energy, 2018; 43(16): 8139-8151 [IF : 4.229]
2 Effect of different wall injection schemes on the flow- field of Hydrogen fuelled strut-based scramjet combustor Acta Astronautica, 2018;145: 93-104 [IF : 2.227] 2017
3 Effect of variation of hydrogen injection pressure and inlet air temperature on the flow-field of a typical double cavity scramjet combustor International Journal of Hydrogen Energy 2017 ; 42(32): 20824-20834 [IF : 4.229]
4 Effect of different strut + wall injection techniques on the performance of two-strut scramjet combustor International Journal of Hydrogen Energy 2017; 42(18): 13259-13275 [IF : 4.229]
5 Effect of parametric variation of strut layout and position on the performance of a typical Two-strut based scramjet combustor International Journal of Hydrogen Energy 2017; 42(15): 10485-10500 [IF : 4.229] 2016
6 Numerical Studies on the Performance of Scramjet Combustor with Alternating Wedge-Shaped Strut Injector International Journal of Turbo & Jet-Engines 2017; 34(1):11–22 [IF : 0.425]
7 Investigation on the effects of operating variables on the performance of two-strut scramjet combustorInternational Journal of Hydrogen Energy 2016; 41(45): 20753–20770 [IF : 4.229]
8 Effect of variation of length- todepth ratio and Mach number on the performance of a typical double cavity scramjet combustor Acta Astronautica 2016; 128 :540-550 [IF : 2.227]
9 Effect of variation of angle of attack on the performance of two-strut scramjet combustor International Journal of Hydrogen Energy 2016; 41(26):11455–11470 [IF : 4.229] 2015
10 Numerical Investigation on Hydrogen-Fueled Scramjet Combustor with Parallel Strut Fuel Injector at a Flight Mach number of 6 Journal of Applied Fluid Mechanics 2016, 9(3):1215-1220 [IF : 1.09]
11 Computational analysis of hypersonic combustor using strut injector at flight Mach 7 Combustion Science and Technology 2015,187 (9):1392-1407 [IF : 1.132]
12 Effect of strut + wall injection techniques on the flowfield of circular-shaped multi-strut scramjet combustorPublished at the 10th International conference on Sustainable Energy and Environmental Protection (SEEP 2017), 27-30 June 2017, in Bled-Slovenia, (Paper ID ; SEEP 258) http://doi.org/10.18690/978-961- 286-058-5.11
13 A brief review on the recent advances in scramjet engine International Conference on Functional Materials, Characterization, Solid State Physics, Power, Thermal and Combustion Energy (FCSPTC-2017) 7-8th April 2017 Andhra Pradesh, India; AIP Conference Proceedings, (AIP) 1859, 020036 (2017) 10.1063/1.4990189
14 Computational Investigation of Heat Transfer Analysis through Perforated Pin Fins of Different Materials International Conference on Functional Materials, Characterization, Solid State Physics, Power, Thermal and Combustion Energy (FCSPTC-2017) 7-8th April 2017 Andhra Pradesh, India); AIP Conference Proceedings 1859, 020009 (2017) 10.1063/1.4990162
15 Analytical Study of Temperature Distribution in a Rectangular Porous Fin Considering both Insulated and Convective Tip International Conference on Functional Materials, Characterization, Solid State Physics, Power, Thermal and Combustion Energy (FCSPTC-2017) 7-8th April 2017 Andhra Pradesh, India; AIP Conference Proceedings 1859, 020031 (2017) 10.1063/1.4990184 2016
16 Composite materials used in Scramjet-A Review International Conference on Processing of Materials, Minerals and Energy (PMME-2016) 29-30 July 2016 Andhra Pradesh, India; Materials Today: Proceedings 5 (2018) 1321–1326
17 Computational simulation of multi-strut central lobed injection of hydrogen in a scramjet combustor International Conference on Recent Trends in Engineering and Material Sciences (ICEMS-2016) 17- 19 March 2016 , Jaipur, India; Perspectives in Science 8(2016) 222-224
18 CFD analysis of rewetting vertical nuclear fuel rod by dispersed fluid jet impingement International Conference on Recent Trends in Engineering and Material Sciences ICEMS-2016) 17-19 March 2016 , Jaipur, India; Perspectives in Science 8(2016)110-112
19 Numerical Investigation of Heat transfer enhancement of SiO2-water based nanofluids in Light water nuclear reactor International Conference on Recent Trends in Engineering and Material Sciences ICEMS-2016) 17-19 March 2016 , Jaipur, India; Materials Today: Proceedings 4(9) (2017) 10118–10122 2014
20 Numerical Investigation of Hypersonic Combustion for a Hydrogen-fueled Scramjet Engine at Flight Mach Number of 7 Proceedings of the 5th International and 41st National Conference on Fluid Mechanics and Fluid Power [FMFP-2014]12- 14th December IIT Kanpur UP India
21 Numerical analysis of Hypersonic Combustion of a Scramjet Combustor with a Central lobed Strut Injector by varying the angle of attack Proceedings ofthe International conference on Innovative Trends in Mechanical, Material, Manufacturing, Automotive, Automobile and Aeronaut