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
 

Downloads

Baseline
External part (STP)

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

 

 

 

Participants
Architect
Integrator
Specialists






Interactive visualization

XDSM Schema

Results

 

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