Use Case – MALE UAV

Top Level Aircraft Requirements
Cruise above civil transport [m]>15000
Payload [kg]800
Range @max Payload [km]>12000
Cruise speed [m/s]150
Dive speed [m/s]180
Landing speed [m/s]55
Take-off field length [m]2500


External part (STP)

CPACS files can be visualized
using TiGLViewer
Fluid meshes
Structural meshesDOE meshes
Flight gear model





Interactive visualization

XDSM Schema



Related Publications

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Walther, J N; Gastaldi, A; Jungo, A; Zhang, M; Maierl, R

Integration Aspects of the Collaborative Aero-Structural Design of an Unmanned Aerial Vehicle Conference

DLRK 2018 , Friedrichshafen, DE, 2018.

Links | BibTeX

Maierl, R; Gastaldi, A; Daoud, F; Walther, J N; Ciampa, P D; Jungo, A; Zhang, M

Aero-Structural Optimization of a Male Configuration in the AGILE MDO Framework Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX

Daoud, F; Dornwald, J; Ernstberger, P; Frantzen, H P; Maierl, R; Deinert, S; Petersen, O

High-Performance Aircraft Through Innovative Development Process and Methods. Conference

AIAA SciTech 2017 , Grapevine, USA, 2017.

Abstract | Links | BibTeX