Use Case – Strut-Braced Wing

Top Level Aircraft Requirements
PAX [-]90
Payload [kg]9180
Range @max Payload [km]3500
Mach number in cruise@ICA [-]0.78
Dive Mach number [-]0.89
Initial cruise altitude [m]11000

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Baseline
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Baseline mesh (IGS/STP)
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Flight gear model

Participants
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Related Publications

Torrigiani, F.; Bussemaker, J.; Ciampa, P. D.; Fioriti, M.; Tomasella, F.; Aigner, B.; Rajpal, D.; Timmermans, H.; Savelyev, A.; Charbonnier, D.

Design of the Strut Braced Wing aircraft in the AGILE Collaborative MDO Framework Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX

Rajpal, D.; Breuker, R. De; Timmermans, H.; Lammen, W.; Torrigiani, F.

Including Aeroelastic Tailoring in the Conceptual Design Process of a Strut Braced Wing Conference

ICAS 2018 , Belo Horizonte, Brazil, 2018.

Links | BibTeX