Hrishikesh Gadgil
Hrishikesh Gadgil
Department of Aerospace Engineering, Indian Institute of Technology Bombay
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Some features of spray breakup in effervescent atomizers
HP Gadgil, BN Raghunandan
Experiments in Fluids 50 (2), 329-338, 2011
Breakup processes of pressure swirl spray in gaseous cross-flow
RS Prakash, H Gadgil, BN Raghunandan
International journal of multiphase flow 66, 79-91, 2014
Numerical assessment of mixing performances in cross-T microchannel with curved ribs
P Borgohain, A Dalal, G Natarajan, HP Gadgil
Microsystem Technologies 24 (4), 1949-1963, 2018
Influence of liquid properties on atomization characteristics of flow-blurring injector at ultra-low flow rates
MA Khan, H Gadgil, S Kumar
Energy 171, 1-13, 2019
Effect of skewness on the characteristics of impinging jet atomizers
H Gadgil, BN Raghunandan
Atomization and Sprays 19 (1), 2009
Delusive influence of nondimensional numbers in canonical hypersonic nonequilibrium flows
S Desai, V Kulkarni, H Gadgil
Journal of Aerospace engineering 29 (5), 04016030, 2016
Aerothermodynamic considerations for energy deposition based drag reduction technique
S Desai, V Kulkarni, H Gadgil, B John
Applied Thermal Engineering 122, 451-460, 2017
Performance assessment of energy deposition based drag reduction technique for Earth and Mars flight conditions
D Das, S Desai, V Kulkarni, H Gadgil
Acta Astronautica 159, 418-428, 2019
Mass distribution studies in effervescent sprays
H Gadgil, A Dolatabadi, BN Raghunandan
Atomization and Sprays 21 (5), 2011
Dynamics of liquid sheet breakup in splash plate atomization
G Thunivumani, H Gadgil
Journal of Fluids Engineering 140 (1), 2018
First step towards atomization at ultra-low flow rates using conventional twin-fluid atomizer
MA Khan, A Katoch, H Gadgil, S Kumar
Experimental Thermal and Fluid Science 109, 109844, 2019
Dynamics of liquid sheet breakup in the presence of acoustic excitation
S Dighe, H Gadgil
International Journal of Multiphase Flow 99, 347-362, 2018
Probing real gas and leading-edge bluntness effects on shock wave boundary-layer interaction at hypersonic speeds
S Desai, S Brahmachary, H Gadgil, V Kulkarni
Journal of Aerospace Engineering 32 (6), 04019089, 2019
Separation mitigation using pressure feedback technique for hypersonic shock wave boundary layer interaction
S Desai, V Kulkarni, H Gadgil
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
Universal scaling parameter for a counter jet drag reduction technique in supersonic flows
S Desai, V Prakash K, V Kulkarni, H Gadgil
Physics of Fluids 32 (3), 036105, 2020
Atomization of acoustically forced liquid sheets
S Dighe, H Gadgil
Journal of Fluid Mechanics 880, 653-683, 2019
Effect of Air Injection Configuration on the Characteristics of Effervescent Sprays
HP Gadgil, BN Raghunandan
Journal of Propulsion and Power 27 (4), 925-928, 2011
Studies On Impinging-Jet Atomizers
HP Gadgil
Effect of transverse acoustic forcing on the characteristics of impinging jet atomization
S Dighe, H Gadgil
Atomization and Sprays 29 (1), 2019
Experimental studies on mass distribution of impinging jets
H Gadgil, S Sabnis, B Raghunandan, C Oommen
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5199, 2006
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