Results 171 to 180 of about 512 (187)

Numerical investigation of cooling performance of 3D-printable cooling structure for aero-engine combustor

Applied Thermal Engineering
Jiahuan Cui, Honglin Li, Yanjia Wang
exaly  

Hydrogen-fueled scramjet cooling system investigation using combustor and regenerative cooling coupled model

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2014
Wen Bao, Weixing Zhou
exaly  

Experimental Studies of Film Cooling in Supersonic Combustors

21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017
Chuan Fan, Jing Wang, Xuejun Fan
openaire   +1 more source

Combustor liner with improved film cooling

2016
CUNHA FRANK J, ERBAS-SEN NURHAK
openaire   +1 more source

A test rig for investigations of gas turbine combustor cooling concepts under realistic operating conditions

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2008
exaly  

Combustor liner with decreased liner cooling

2015
CUNHA FRANK J, ERBAS-SEN NURHAK
openaire   +1 more source

Combustor cooling with angled segmented surfaces

2008
BUNKER RONALD SCOTT, BAILEY JEREMY CLYDE, WIDENER STANLEY KEVIN, JOHNSON THOMAS EDWARD   +3 more
openaire   +1 more source

Combustor liner with convergent cooling channel

2016
CUNHA FRANK J, ERBAS-SEN NURHAK
openaire   +1 more source

Advanced Gas Turbine Combustor Cooling Configurations

Proceedings of the 1992 International Symposium on Heat Transfer in Turbomachinery, 1994
openaire   +1 more source

Combustor cooling for gas turbine engines

1995
openaire   +3 more sources