Use Case – Innovative Turboprop (wing-mounted engines)

Top Level Aircraft Requirements
PAX [-]90
Payload [kg]9540
Range @max Payload [km]2222
Mach number in cruise@7620m [-]0.56
Maximum operating altitude [m]7620
Take-off field length [m]1500
Fuselage diameter [m]3.53


Baseline optimized
Baseline with engines

CPACS files can be visualized
using TiGLViewer

TP-RMwith movables (STP)
Flight gear model


Interactive visualization

XDSM Schema

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



Related Publications

Stingo, L.; Vecchia, P. Della; Cerino, G.

MDO Applications to Conventional and Novel Turboprop Aircraft within the AGILE European Project Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX

Vecchia, P. Della; Stingo, L.; Nicolosi, F.; Cerino, G.; Ciampa, P. D.; Prakasha, P. S.; Fioriti, M.; Zhang, M.; Mirzoyan, A.; Aigner, B.; Charbonnier, D.

Advanced Turboprop Multidisciplinary optimization within AGILE project Conference

vol. paper 2018-3205, AIAA Aviation 2018 , Atlanta, US, 2018.

Links | BibTeX

Mirzoyan, A.; Isyanov, A.; Cerino, G.; Vecchia, P. Della; Stingo, L.; Fioriti, M.; Boggero, L.; Tomasella, F.; Prakasha, P. S.

Comparative study of advanced turboprop aircraft with wing and rear mounted propulsion system in the AGILE EU project Conference

vol. paper 2018-2849, AIAA Propulsion & Energy 2018 , Atlanta, US, 2018.

Links | BibTeX