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
 

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BWB-Baseline
BWB-winglets

CPACS files can be visualized
using TiGLViewer

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

 

 

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Interactive visualization

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Related Publications

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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

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