Conjugate Heat Transfer Simulation of a Subscale Rocket Thrust Chamber Using a Timescale Based Frozen Non-Adiabatic Flamelet Combustion Model
AIAA Propulsion and Energy 2019 Forum
American Institute of Aeronautics and Astronautics
2019
An experimental and modelling study of heat loads on a subscale methane rocket motor
Acta Astronautica
2019
164
112-120
Temperature and Size Measurements of Cryogenic Spray Droplets with Global Rainbow Refractometry
Journal of Propulsion and Power
2019
35
2
359-368
Experimental Investigations of Thermomechanical Fluid–Structure Interaction in Rocket Combustion Chambers
Journal of Propulsion and Power
2019
35
5
906-916
Heat Transfer and Combustion Simulation of Seven-Element O2/CH4 Rocket Combustor
Journal of Propulsion and Power
2019
35
6
1080-1097
Heat flux evaluation in a multi-element CH4/O2 rocket combustor using an inverse heat transfer method
International Journal of Heat and Mass Transfer
2019
142
118425
Conjugate Heat Transfer Simulation of a Subscale Rocket Thrust Chamber Using a Timescale Based Frozen Non-Adiabatic Flamelet Combustion Model
55th AIAA/SAE/ASEE Joint Propulsion Conference, Indianapolis, Indiana, USA
2019
Generation of non-adiabatic flamelet manifolds: comparison of two approaches applied on a single-element GCH4/GO2 combustion chamber
EUCASS 2019
2019