Multi-Fidelity Aerodynamic Surrogate Modeling for Conceptual Design Using GNNs
Invited talk, NASA Advanced Modeling and Simulation (AMS) Seminars, Moffett Field, CA, USA
Conceptual aircraft design requires major engineering decisions under limited information. In practice, low-fidelity aerodynamic tools are routinely used because higher-fidelity simulations are often unavailable or too expensive for early-stage design. This creates a fidelity-cost gap: the level of analysis fidelity needed for confident decision-making is not available at the stage with the greatest downstream impact. This challenge is especially important in supersonic transport design, where nonlinear aerodynamic effects make considerations such as low-speed stability difficult to assess using conventional conceptual design tools.
