Use Case – Blended Wing Body

Top Level Aircraft Requirements
PAX [-]450
Payload [t]59
Range @max Payload [km]8500
Mach number in cruise@ICA [-]0.85
Maximum operating altitude [ft]43000
Approch speed (@MLW, SL, ISA) [kts]166
Take-off field length [m]2950

Downloads

Baseline

CPACS files can be visualized
using TiGLViewer

BWB (SU2)
BWB-winglets (SU2)
BWB-winglets-nacelles (STP/CGNS)
BWB-winglets-nacelles-pylons (STP)
Flight gear model

Participants
Architect
Integrator
Specialists









Interactive visualization

Results

Related Publications

Prakasha, P. S.; Ciampa, P. D.; Vecchia, P. Della; Ciliberti, D.; Voskuijl, M.; Charbonnier, D.; Jungo, A.; Fioriti, M.; Anisimov, K.; Mirzoyan, A.

Multidisciplinary Design Analysis of Blended Wing Body through Collaborative Design Approach: AGILE EU Project Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX

Mirzoyan, A.; Isyanov, A.; Fioriti, M.; Boggero, L.; Tomasella, F.; Prakasha, P. S.; Ciampa, P. D.

Propulsion System for BWB configurations in the AGILE project Conference

paper 2018-2848 , AIAA Propulsion & Energy 2018 , Atlanta, US, 2018.

Links | BibTeX