Design an airliner the way Airbus and Boeing start one
Every design is a whole single-aisle airliner (A320 / 737 class): the wing's airfoil (6 shape parameters, learned from OpenFOAM by a graph network), its area, aspect ratio, taper, sweep, twist and position, and the cruise Mach. Each one flies its mission (cruise at Mach 0.70–0.82, approach and landing) and goes through a design review:
Less impactg of CO₂ per passenger-km over the design mission (Breguet, turbofan fuel burn)
Fastercruise Mach, with the wave drag of the shocks that come with it (Korn equation)
Lands slowerapproach speed with slats and flaps: shorter runways, less noise
Certifiable36 m gate span, 1.3 g buffet margin, fuel in the wing, static margin, stall at the root, trim
The reference is an A320ceo-class airliner (wing 122.6 m², span 34.1 m, 25° sweep, Mach 0.78) with a conventional NACA 2412 section.
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API
Run the search, evaluate a design, get its flow field or a ready OpenFOAM case. Interactive documentation: /docs.
Python (PINNeAPPle)