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Ramakrishna Periyapatna
Ramakrishna Periyapatna
Department of Aerosace Engineering IIT Madras
Verified email at iitm.ac.in - Homepage
Title
Cited by
Cited by
Year
Studies on the role of iron oxide and copper chromite in solid propellant combustion
K Ishitha, PA Ramakrishna
Combustion and Flame 161 (10), 2717-2728, 2014
892014
Sandwich propellant combustion: Modeling and experimental comparison
PA Ramakrishna, PJ Paul, HS Mukunda
Proceedings of the Combustion Institute 29 (2), 2963-2973, 2002
862002
Effect of mechanical activation of high specific surface area aluminium with PTFE on composite solid propellant
M Gaurav, PA Ramakrishna
Combustion and Flame 166, 203-215, 2016
702016
Towards the development of a high power density, high efficiency, micro power generator
B Aravind, B Khandelwal, PA Ramakrishna, S Kumar
Applied Energy 261, 114386, 2020
542020
Ageing studies on AP/HTPB based composites solid propellants
H Naseem, J Yerra, H Murthy, PA Ramakrishna
Energetic Materials Frontiers 2 (2), 111-124, 2021
472021
Studies on EVA‐Based Wax Fuel for Launch Vehicle Applications
R Kumar, PA Ramakrishna
Propellants, Explosives, Pyrotechnics 41 (2), 295-303, 2016
442016
Innovative design to improve the power density of a solid oxide fuel cell
PA Ramakrishna, S Yang, CH Sohn
Journal of Power Sources 158 (1), 378-384, 2006
442006
Effect of specific surface area of aluminum on composite solid propellant burning
S Verma, PA Ramakrishna
Journal of Propulsion and Power 29 (5), 1200-1206, 2013
422013
Enhancement of hybrid fuel regression rate using a bluff body
R Kumar, PA Ramakrishna
Journal of Propulsion and Power 30 (4), 909-916, 2014
412014
An effective method to embed catalyst on AP and its effect on the burn rates of aluminized composite solid propellants
G Marothiya, C Vijay, K Ishitha, PA Ramakrishna
Combustion and Flame 182, 114-121, 2017
382017
Issues Related to the Measurement of Regression Rate of Fast-Burning Hybrid Fuels
R Kumar, PA Ramakrishna
Journal of Propulsion and Power 29 (5), 1114-1121, 2013
372013
Estimation of burning characteristics of AP/HTPB composite solid propellant using a sandwich model
C Vijay, PA Ramakrishna
Combustion and Flame 217, 321-330, 2020
362020
Measurement of regression rate in hybrid rocket using combustion chamber pressure
R Kumar, PA Ramakrishna
Acta Astronautica 103, 226-234, 2014
362014
Combustion of sandwich propellant at low pressures
PA Ramakrishna, PJ Paul, HS Mukunda, CH Sohn
Proceedings of the Combustion Institute 30 (2), 2097-2104, 2005
342005
Effect of protrusion on the enhancement of regression rate
R Kumar, PA Ramakrishna
Aerospace Science and Technology 39, 169-178, 2014
322014
Dependence of density and burning rate of composite solid propellant on mixer size
S Verma, PA Ramakrishna
Acta Astronautica 93, 130-137, 2014
292014
Activated charcoal–A novel burn rate enhancer of aluminized composite propellants
S Verma, PA Ramakrishna
Combustion and Flame 157 (6), 1202-1210, 2010
292010
Investigations on activated charcoal, a burn-rate enhancer in composite solid propellant
S Verma, PA Ramakrishna
Journal of Propulsion and Power 29 (5), 1214-1219, 2013
232013
Experimental investigation of temperature separation in a counter-flow vortex tube
PA Ramakrishna, M Ramakrishna, R Manimaran
Journal of heat transfer 136 (8), 082801, 2014
222014
Combustion of Ammonium Perchlorate monopropellant: Role of heat loss
K Nagendra, C Vijay, M Ingole, PA Ramakrishna
Combustion and Flame 209, 363-375, 2019
212019
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