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Proc. ASME. GT2021, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture, V001T01A007, June 7–11, 2021
Paper No: GT2021-58945
..., Germany Email: email@example.com ABSTRACT Keywords: Aeronautics, Combustor, Optimization, Aero- The preliminary design of an aero-engine combustor is a thermal, Design Automation, Methodology multidisciplinary process that involves an extensive and systematic NOMENCLATURE analysis...
Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A033, September 21–25, 2020
Paper No: GT2020-16003
... analysis within the loop and the enhancement of the procedure s robustness. In this paper will be presented the Combustor Design System Integration (DSI), a methodology aimed at easing and streamlining the design process of aero-engine combustors. To do this, digitization has been taken as the common...
Proc. ASME. GT2013, Volume 6B: Turbomachinery, V06BT37A037, June 3–7, 2013
Paper No: GT2013-95469
... role in early design stages. The aim of this paper was to present the methodology of mean-line designing of axial turbines and to discuss the computational methods and procedures used. The paper presents the Lund University Axial Turbine mean-line code (LUAX-T). LUAX-T is a reduced- order through-flow...