Use Case – Strut-Braced Wing

Top Level Aircraft Requirements
PAX [-]90
Payload [kg]9180
Range @max Payload [km]3500
Mach number in cruise@ICA [-]0.78
Dive Mach number [-]0.89
Initial cruise altitude [m]11000
 

Downloads

Baseline
Baseline with engines
Min DOC

CPACS files can be visualized
using TiGLViewer
Baseline mesh (IGS/STP)
Min DOC mesh (IGS/STP)
Flight gear model

 

 

 

Participants
Architect
Integrator
Specialists








 

Interactive visualization

XDSM Schema

You can download the CMDOWS file of this XDMS Schema and open it with the MDO System Interface to see it in details.

 

Results

 

Related Publications

Torrigiani, F; Bussemaker, J; Ciampa, P D; Fioriti, M; Tomasella, F; Aigner, B; Rajpal, D; Timmermans, H; Savelyev, A; Charbonnier, D

Design of the Strut Braced Wing aircraft in the AGILE Collaborative MDO Framework Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX

Rajpal, D; De Breuker, R; Timmermans, H; Lammen, W; Torrigiani, F

Including Aeroelastic Tailoring in the Conceptual Design Process of a Strut Braced Wing Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX