Abstract: Although the benefits of intercooling for aeroengine applications have been realized and discussed in many publications, quantitative details are still relatively limited. In order to strengthen the understanding of ...

Abstract: The reduction of CO2 emissions is strongly linked with the improvement of engine specific fuel consumption, along with the reduction of engine nacelle drag and weight. One alternative design approach to improving specific ...

Abstract: Despite the need for highly qualified experts, multidisciplinary gas turbine conceptual design has not been a common study topic in traditional postgraduate curriculums. Although many courses on specialized topics in gas ...

Abstract: The aim of this study was to compare singleand twinshaft oxyfuel gas turbines in a semiclosed oxyfuel combustion combined cycle (SCOC–CC). This paper discussed the turbomachinery preliminary meanline design of oxyfuel ...

Abstract: An optimal baseline turbofan cycle designed for a performance level expected to be available around year 2050 is established. Detailed performance data are given in takeoff, top of climb, and cruise to support the analysis. ...