Results 111 to 120 of about 480,813 (179)
Some of the next articles are maybe not open access.
Numerical Heat Transfer, Part A: Applications, 2020
The structural optimization of a specific laminated cooling structure is conducted under gas turbine combustor representative aero-thermal conditions, with the aim at improving its overall cooling ...
Chen Wang +3 more
openaire +2 more sources
The structural optimization of a specific laminated cooling structure is conducted under gas turbine combustor representative aero-thermal conditions, with the aim at improving its overall cooling ...
Chen Wang +3 more
openaire +2 more sources
Superposition of Overall Cooling Effectiveness on a Turbine Blade Leading Edge
Volume 7: Heat Transfer: Combustors; Heat Transfer: Film CoolingAbstract Increasingly harsh turbine environments necessitate the design of more advanced cooling techniques as well as prediction of those cooling schemes’ performance at engine conditions. For several decades, film cooling design has been accelerated through a low-order superposition of adiabatic effectiveness in order to quickly ...
Bailey W. Hopkins, James L. Rutledge
openaire +2 more sources
Overall Cooling Effectiveness of Internally Cooled Additively Manufactured Blades
Conference Name: industryXchange 2025: Energy Location: State College, PA Start Date: 5/20/2025 12:00:00 AM End Date: 5/21/2025 12:00:00 AMRachel Ross +5 more
semanticscholar +3 more sources
Volume 5A: Heat Transfer, 2019
Abstract The previous theoretical work showed the matching principles of analogy parameters for effusion-impingement cooling model. The mismatch of temperature ratios Tg/Tc may result in different matching performance in laboratory condition.
Gang Xie +4 more
openaire +2 more sources
Abstract The previous theoretical work showed the matching principles of analogy parameters for effusion-impingement cooling model. The mismatch of temperature ratios Tg/Tc may result in different matching performance in laboratory condition.
Gang Xie +4 more
openaire +2 more sources
Experimental investigation on the overall cooling effectiveness of t-type impinging-film cooling
Applied Thermal Engineering, 2018Abstract This paper presents an experimental investigation of impinging-film cooling concerning the effects of various factors on overall cooling effectiveness η. The factors include blowing ratio M (0.31 ≤ M ≤ 1.84), non-dimensional jet-to-plate pitch Zn/d (1 ≤ Zn/d ≤ 2), non-dimensional spacing of jet holes Yn/d (1.6 ≤ Yn/d ≤ 2.4) and diameter of ...
Jingyu Zhang +4 more
openaire +2 more sources
Overall cooling effectiveness of effusion cooled annular combustor liner at reacting flow conditions
Applied Thermal Engineering, 2018Abstract A three-sector annular combustor test rig is built to carry out experimental investigation on the liner effusion cooling performance using steady state infrared radiation thermography method at reacting flow conditions. 7 rows of effusion holes in a staggered layout are distributed on both inner and outer liner bended testing plates, where ...
Yongbin Ji +3 more
openaire +2 more sources
International Journal of Heat and Mass Transfer, 2018
Abstract The overall cooling effectiveness, which represents the distribution of dimensionless temperature on gas turbines surface, is an important parameter for conjugate heat transfer analysis of gas turbines. Generally, it is difficult to measure the overall cooling effectiveness in engine condition.
Cun-liang Liu +3 more
semanticscholar +3 more sources
Abstract The overall cooling effectiveness, which represents the distribution of dimensionless temperature on gas turbines surface, is an important parameter for conjugate heat transfer analysis of gas turbines. Generally, it is difficult to measure the overall cooling effectiveness in engine condition.
Cun-liang Liu +3 more
semanticscholar +3 more sources

