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; De Breuker, R; 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