Due to the instability of the pitching moment induced by the strong vortical flow at moderate
to high angles of attack in the unmanned combat aerial vehicle (UCAV) configuration …

This work presents a multi-fidelity aerodynamic modeling approach for the aerodynamic
model generation of the NATO AVT–251 Task Group's UCAV configuration named …

The analysis, design, and simulation of complex systems such as aircraft require the use of a
multitude of software tools from a wide range of disciplines. While each disciplinary tool …

This article describes the aerodynamic design and assessment of a UCAV wing developed
under the NATO-STO AVT-251 Multi-disciplinary Design Task Group. The wing design …

Turbulence models based on Reynolds-averaged Navier-Stokes (RANS) equations remain
the workhorse in the computation of high Reynolds-number wall-bounded flows. While these …

Purpose This paper aims to present a literature review on analytical research on the
prediction of aircraft spin and recovery characteristics, as it progressed from the early years …

II. Introduction he subject of Unmanned Combat Air Vehicle (UCAV) wing design has and
continues to be a major research and development activity. Many manufacturers throughout …

This article belongs to a series of publications on the design and assessment of the
MULDICON UCAV configuration. MULDICON is a 53° swept flying wing combat aircraft …

View Video Presentation: https://doi. org/10.2514/6.2023-3515. vid The aim of the DLR
research project Diabolo is to digitalize the classic methods of conceptual combat aircraft …

The design of highly swept flying wing UCAV 3 configurations is a complex task. Due to a
high level of integration in combination with vortex-dominated flow structures, the application …