Injector Dynamics and Pressure Gain in Rotating Detonation Engines.- Low Emissions Propulsion Engine Characterization Process.- Aerodynamic and Aero-Acoustic Performance of an Adjustable Pitch Axial Flow Fan.- Proposed Thrust Profile Design of Pulse Detonation Engine (PDE) for Aerospace Applications.- The Formation of PAH Compounds from the Combustion of Biofuels.- Review of Biomass Energy Resources with Livestock Manure.- Higher Alcohols as Diesel Engine Fuel.- Photocatalytic Hydrogen from Water over Semiconductors.- Evaluation of Hazard Correlations for Hydrogen Rich Fuels using Stretched Transient Flames.- Experimental Investigation of Turbulent Flow/Flame Structure of Double Swirler Burner.
Dr. Ashwani K. Gupta is a Distinguished University
Professor at the University of Maryland (UMD), USA. He obtained his
Ph.D. and D.Sc. from the University of Sheffield, UK. He was
awarded D.Sc. from Southampton University, UK, and Honorary
Doctorates from the University of Wisconsin–Milwaukee, USA, King
Mongkut’s University of Technology North Bangkok, Thailand, and
University of Derby, UK. He received the President Kirwan Research
Award and College of Engineering Research Award at UMD. He has
received several honors and awards from AIAA and ASME, and has
co-authored over 800 papers, 3 books, 5 patents, and edited 18
books in the areas of combustion, swirl flows, high temperature air
combustion (HiTAC), distributed combustion, wastes to energy, acid
gas treatment, fuel reforming, and air pollution. He is Honorary
Fellow of ASME and RAeS (UK), and Fellow of AIAA, SAE, and
AAAS.
Dr. Ashoke De is a Professor in the Department of
Aerospace Engineering, Indian Institute of Technology (IIT) Kanpur.
He received his MS from IIT Kanpur, and Ph.D. from Louisiana State
University, USA. Before joining IIT Kanpur, he has worked as
post-doctoral scholar at Technical University of Delft (TU-Delft),
Netherlands and as Research Engineer in GE Global research at
Bangalore, India. He is the recipient of DAAD Fellowship (2016),
IEI-Young Engineer’s Award-2014 (Aerospace Engineering), Early
Career Research award-2015 (DST, India), Expertise Award-2010 (GE
Global research), and P K Kelkar Young Research Fellowship
(2015-2018, IITK). He is AvHumboldt Fellow, Fellow of West Bengal
Academy of Science and Technology, Associate Editor of
International Journal of Energy for a Clean Environment
(2019-present), and currently member of APS, AIAA (senior member),
ASME, SIAM, FMFP, ISHMT and Combustion Institute. He leads large
scale initiatives in the modelling of turbulent flows at IIT Kanpur
and authored over 130 papers, and 4 edited books. His current
research interests include multiphase modeling, hybrid RANS/LES
model development, supersonic flows and Fluid-Structure
interactions (FSI).
Dr. Suresh K. Aggarwal received his Ph.D. from Georgia Institute of Technology, Atlanta, USA. He was a member of the research staff at Princeton University, New Jersey, USA and a Senior Research Engineer at CMU. He then joined the University of Illinois at Chicago, USA and was promoted to Professor in 1995. He served as Director of Graduate Studies, and was also a Visiting Scientist at ANL, Visiting Professor at Ecole Centrale-Paris, France and Guest Professor at Jiangsu University, China. His research interests include Combustion, Multiphase Reacting Flows, Emissions, Clean Energy, and Fire Suppression. He has authored over 340 publications and graduated 17 Ph.D. and 46 MS students. He is Fellow of ASME, AAAS and Associate Fellow of AIAA.
Dr. Abhijit Kushari is Professor in the Department of
Aerospace Engineering, Indian Institute of Technology (IIT) Kanpur,
India. Dr. Kushari received his Ph.D. from Georgia Institute of
Technology, Atlanta, Georgia, in 2000 and joined IIT Kanpur as an
Assistant Professor in 2001. He became a Professor in 2014. His
research interests are Aerospace Propulsion, Gas Turbine engines,
Turbo-machinery, Liquid Atomization Flow Control and Combustion
Dynamics. He has authored more than 130 technical papers. He has
supervised 6 PhD and 50 M.Tech theses in Aerospace Propulsion
fields.
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