Parametric Optimization for Advanced Aircraft Conceptual Design

Aircraft designers manually iterate through dozens of design variables—wing sweep, aspect ratio, taper ratio, fuselage geometry, inlet shape—hoping to find configurations that meet multiple competing objectives. Traditional optimization requires exporting to separate tools, building complex data pipelines, and running disconnected workflows that take days to set up and break with each design change. This trial-and-error approach wastes weeks on design space exploration that should be systematic and objective-driven.

Join us to see how nTop eliminates this complexity with built-in inverse design optimization—define what you want to achieve and let nTop automatically explore design variations to meet your goals, all within the parametric modeling environment.

What you’ll see:

• Built-in optimization algorithms – Choose an optimization method and work directly on parametric implicit models with any quantifiable result as an objective—no separate tools or exports required
• Multi-variable aircraft configuration optimization – Watch nTop automatically explore wing parameters for maximizing fuel capacity and structural rigidity across the design space
• CFD- and FEA-driven optimization – Optimization using nTop Fluids CFD results where analysis runs automatically for each iteration without meshing bottlenecks
• Complete workflow demonstration – From defining objectives and design variables through convergence analysis to comparing baseline and optimized configurations

Can’t attend live? No problem. Register today and we’ll send you a copy of the recording when it’s available.