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 |
|
TP-RM (STP) TP-RMwith movables (STP) |
|
Flight gear model |
Interactive visualization
XDSM Schema
Loading...
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
MDO Applications to Conventional and Novel Turboprop Aircraft within the AGILE European Project Conference
ICAS 2018 , Belo Horizonte, Brazil, 2018.
Advanced Turboprop Multidisciplinary optimization within AGILE project Conference
vol. paper 2018-3205, AIAA Aviation 2018 , Atlanta, US, 2018.
vol. paper 2018-2849, AIAA Propulsion & Energy 2018 , Atlanta, US, 2018.
You must be logged in to post a comment.