ResearchBenchmarksAerodynamic Design Optimization on Airfoil Cl/Cd B=100Aerodynamic Design Optimization on Airfoil Cl/Cd B=100Follow180.46Best Objective Value (Median)SPARROW128.2141.7675155.335168.9025Jul 1, 2026Evaluation resultsMethodMethodLinksBest Objective Value (Median)Best Objective Value (IQR)SPARROWBudget (B)=100Budget (B)=1002026.07180.46179.13GPBudget (B)=100Budget (B)=1002026.07158.85139.2CMA-ESBudget (B)=100Budget (B)=1002026.07152.65146.67RDSBudget (B)=100Budget (B)=1002026.07142.1127.46TuRBOBudget (B)=100Budget (B)=1002026.07130.21122.88