Aile Haubanée vs Aile cantilever dans le cadre d'une propulsion LH2 : Compromis aéro-structure et Challenges

Key Points

• The study identifies key compromises in aerodynamic efficiency and structural integrity between the haubanée and cantilever wing designs.
• Aerodynamic assessments reveal that the haubanée wing design may enhance stability while increasing complexity in structural materials.
• Comparative analysis involved simulations and theoretical models to evaluate performance metrics across distinct flight scenarios.
• Findings suggest that selecting the optimal wing design for LH2 propulsion involves balancing aerodynamic benefits against structural challenges.