In the German Aerospace Center's Virtual Aircraft Technology Integration Platform project, a
process for aerostructural wing optimization based on high-fidelity simulation methods is …

This work presents the application of a recently developed parametric, non-intrusive, and
multi-fidelity reduced-order modeling method on high-dimensional displacement and stress …

View Video Presentation: https://doi. org/10.2514/6.2021-3080. vid This paper presents a
certification-driven design process for an Unmanned Medium-Altitude-Long-Endurance …

In this paper, a knowledge-based approach to support analysis model generation is
proposed, which aims to improve consistency among the models used by different …

Distributed electric propulsion (DEP) concepts leverage the synergistic benefits of
aeropropulsive coupling and improve the overall flight efficiency by placing propulsors at …

View Video Presentation: https://doi. org/10.2514/6.2021-2448. vid The conceptual design
phase traditionally employs the “tail volume ratio” method to initially size the horizontal and …

View Video Presentation: https://doi. org/10.2514/6.2022-3204. vid The Parallel Electric-Gas
Architecture with Synergistic Utilization Scheme (PEGASUS) is a regional aircraft concept …

Airworthiness certification is challenging for novel aircraft concepts. To avoid the significant
cost associated with the redesign for certification compliance, incorporating certification …

Aircraft design optimization traditionally relies on computationally expensive simulation
techniques such as Finite Element Method (FEM) and Finite Volume Method (FVM), which …