Objective:Design of ultra-efficient ‘dry’ wing for the targeted SR/SMR aircraft concept exploiting non-drop-in fuels such as hydrogen, including optimized solutions for unducted engine integration, aerodynamic optimisation and flutter management. Maturation at TRL4 or higher via ground and scaled-flight tests demonstration by project completion. For the full description of this topic please download the PDF document of the topics from the "Additional Documents" section.
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