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 meshes

DOE meshes

Flight gear model


Interactive visualization

XDSM Schema

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Related Publications

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