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
 

Downloads

Baseline
Baseline optimized
Baseline with engines

CPACS files can be visualized
using TiGLViewer
TP-RM (STP)
TP-RMwith movables (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

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

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

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX

Della Vecchia, P; 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

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

Links | BibTeX

Mirzoyan, A; Isyanov, A; Cerino, G; Della Vecchia, P; 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

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

Links | BibTeX