The aim of this review paper is to collect and discuss the most relevant and updated
contributions in the literature regarding studies on new or non-conventional technologies for …

In a time when low emission solutions and technologies are of utmost importance regarding
the sustainability of the aviation sector, this publication introduces a reduced-order physics …

An approach for preliminary aero-engine design, incorporating a mean-line code for the
design of axial-flow, multi-stage compressors, is presented. The compressor mean-line code …

Disks in gas turbines are optimized for minimum weight, while satisfying both geometry and
stress constraints, in order to minimize the engine production, operation, and maintenance …

The present research work focuses on accurate aerodynamic computation and flow
investigations of NACA 4-digit airfoil design to enhance the lift performance and …

Currently projected supersonic business jets target selected supersonic flight missions with
Mach numbers of about 1.4 and a larger number of long-range subsonic flight missions …

In this paper, robustness optimization of a fatigue-critical welded structure with measured
misalignments and a generic robust design procedure are presented. The motivation for …

As energy transition to alternative fuels for civil aviation is likely to be gradual, hydrogen's
first entry to service may be implemented on existing gas turbine engines. In this paper a …

In the conceptual design process of aeroengines, the thermal parameters and the
fundamental structure must be determined. To reduce iterative adjustments between the …

Mission-adaptive aerostructural design considers the alteration of structural geometries to im-
prove multi-objective performance in multiple aerodynamic environments. Geometric …