Use Case – Blended Wing Body (boundary layer ingestion)

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

BWB-Baseline
BWB-winglets

CPACS files can be visualized
using TiGLViewer

BWB-winglets-BLI (STP)
Mesh BWB-winglets-nacelles (CGNS)

Participants
Architect
Integrator
Specialists





Interactive visualization

Results

Related Publications

Prakasha, P S; Ciampa, P D; Della Vecchia, P; 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