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Effusion cooling in rocket combustors applying fibre reinforced ceramics

35th Joint Propulsion Conference and Exhibit, 1999
Since 1994 DLR has focused its efforts on combustion chamber technologies within the internal program "High Pressure Rocket Propulsion" (HDR). The main emphasis lays on advanced cooling technologies and especially effusion cooling applying fibre reinforced ceramics as porous media and hydrogen as cooling fluid.
Serbest, E.   +4 more
openaire   +2 more sources

Effusion Cooling System Optimization for Modern Lean Burn Combustor

Volume 5B: Heat Transfer, 2016
Stricter legislation limits concerning NOx emissions are leading main aero-engine manufacturers to update the architecture of the combustors towards the implementation of lean burn combustion concept. Cooling air availability for the thermal management of combustor liners is significantly reduced, demanding even more effective liner cooling schemes ...
Andreini, Antonio   +5 more
openaire   +1 more source

Numerical study of effusion cooling of a gas turbine combustor liner

Fuel, 2021
Jin Wang, Liang Tian, Jakov Baleta
exaly  

A machine learning approach to quantify the film cooling superposition effect for effusion cooling structures

International Journal of Thermal Sciences, 2021
Li Yang, Yu Rao, Minking K Chyu
exaly  

Experimental investigation of effusion and transpiration air cooling for single turbine blade

Applied Thermal Engineering, 2021
MinGeon Kim   +2 more
exaly  

Numerical investigation of jet array impingement cooling with effusion holes

Applied Thermal Engineering, 2021
Won-Woo Choi, Sung-Min Kim
exaly  

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