Aeropropulsive Shape Optimization of an Airfoil System in the Transonic Regime
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MG Lauer, PJ Ansell
Journal of Aircraft, 2025
arc.aiaa.org
Boundary-layer ingestion and distributed propulsion are important concepts for future aircraft systems and technologies. Both concepts have the potential to increase aerodynamic efficiency and improve aircraft design in various other ways. The present study aims to address design implications and challenges of configuring a highly integrated and distributed propulsion system into wing sections within the compressible flow environment, which is the aerodynamic regime associated with large, commercial transport aircraft. To this …
