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Kanmaniraja Radhakrishnan
Kanmaniraja Radhakrishnan
Department of Aerospace Engineering, Inha University
Verified email at inha.ac.kr
Title
Cited by
Cited by
Year
Numerical study on the combustion characteristics of a fuel-centered pintle injector for methane rocket engines
M Son, K Radhakrishnan, Y Yoon, J Koo
Acta Astronautica 135, 139-149, 2017
782017
Design procedure of a movable pintle injector for liquid rocket engines
M Son, K Radhakrishnan, J Koo, OC Kwon, HD Kim
Journal of Propulsion and Power 33 (4), 858-869, 2017
762017
Effect of injection conditions on mixing performance of pintle injector for liquid rocket engines
K Radhakrishnan, M Son, K Lee, J Koo
Acta Astronautica 150, 105-116, 2018
442018
Verification on spray simulation of a pintle injector for liquid rocket engine
M Son, K Yu, K Radhakrishnan, B Shin, J Koo
Journal of thermal science 25 (1), 90-96, 2016
362016
Lagrangian approach to axisymmetric spray simulation of pintle injector for liquid rocket engines
K Radhakrishnan, M Son, K Lee, J Koo
Atomization and Sprays 28 (5), 2018
182018
3D numerical studies on jets acoustic characteristics of chevron nozzles for aerospace applications
R Kanmaniraja, R Freshipali, J Abdullah, K Niranjan, K Balasubramani, ...
International Journal of Aerospace and Mechanical Engineering 8 (9), 1530-1536, 2014
162014
Computational and theoretical analysis of aerodynamic performance on roller airfoil
MS Kumar, R Vijayanandh, N Kaviarasan, RD Kumar, IAI Arasu, ...
International Journal of Engineering & Technology 7 (4.10), 637-642, 2018
112018
A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines
K Radhakrishnan, K Lee, J Koo
Combustion Theory and Modelling 25 (4), 718-750, 2021
92021
Multi-fidelity surrogate models for predicting averaged heat transfer coefficients on endwall of turbine blades
W Choi, K Radhakrishnan, NH Kim, JS Park
Energies 14 (2), 482, 2021
52021
Volume of fluid simulation of sheet formation and primary breakup of non-newtonian propellants in a pintle injector with variable injection areas
K Radhakrishnan, J Koo, Y Hwang
Atomization and Sprays 30 (2), 2020
52020
R. Kanmani raja, Computational and Theoretical Analysis of Aerodynamic Performance on Roller Airfoil, October 2018
MS Kumar, R Vijayanandh, N Kaviarasan, RD Kumar, IAI Arasu
International Journal of Engineering & Technology 7 (4.10), 637-642, 2018
52018
Effect of internal flow guide in pintle tip on pintle injector thruster combustion
K Lee, J Nam, K Radhakrishnan, J Koo
Journal of the Korean Society for Aeronautical & Space Sciences 48 (9), 703-709, 2020
42020
Thermal analysis and creep lifetime prediction based on the effectiveness of thermal barrier coating on a gas turbine combustor liner using coupled CFD and FEM simulation
K Radhakrishnan, JS Park
Energies 14 (13), 3817, 2021
32021
Spray Characteristics of Jet According to Position of Injector Hole in Crossflow
MH Choi, DS Shin, K Radhakrishnan, M Son, J Koo
Journal of the Korean Society of Propulsion Engineers 22 (5), 88-96, 2018
22018
Effects of propellant phases on atmospheric spray characteristics of a pintle injector for throttleable rocket engines
K Yu, M Son, K Radhakrishnan, HD Kim, J Koo
Journal of ILASS-Korea 21 (1), 13-19, 2016
22016
Investigation on Thermally Damaged Thrust Chamber wall by Improper Film Cooling in Small-Scale GCH4/GOX Rocket Engines Using CFD Simulations
K Radhakrishnan, J Shin, HJ Lee
한국항공우주학회 학술발표회 초록집, 285-286, 2024
2024
Flow and Heat Transfer Characteristics of Superheater Tube of a Pulverized Coal-Fired Boiler Using Conjugate Heat Transfer Modeling
K Radhakrishnan, JS Park
Energies 17 (5), 1161, 2024
2024
Impact of Radiation on Conjugate Heat Transfer Analysis in Primary Superheater of a Pulverized Coal Boiler using CFD
K Radhakrishnan, JS Park
유체기계 연구개발 발표회 논문집, 320-321, 2021
2021
Multi-Fidelity Surrogate Models for Predicting Averaged Heat Transfer Coefficients on Endwall of Turbine Blades. Energies 2021, 14, 482
W Choi, K Radhakrishnan, NH Kim, JS Park
s Note: MDPI stays neutral with regard to jurisdictional claims in published …, 2021
2021
핀틀 인젝터의 팁 내부 유동 가이드가 연소 성능에 미치는 영향; 핀틀 인젝터의 팁 내부 유동 가이드가 연소 성능에 미치는 영향; Effect of Internal Flow Guide in Pintle Tip on Pintle …
K Lee, J Nam, K Radhakrishnan, J Koo
Journal of the Korean Society for Aeronautical & Space Sciences 48 (9), 703-709, 2020
2020
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