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The NextWing project focuses on developing advanced three-dimensional shock control bumps to enhance the performance of laminar wings in future transport aircraft. By improving drag reduction at high speeds, the project aims to increase eco-efficiency in aviation.
The utilization of laminar flow technology is one necessary mean to further improve the eco-efficiency of future transport aircraft.
Because of the different pressure distribution type and the reduced sweep of laminar wings the drag rise is encountered at lower Mach numbers and is steeper than with conventional turbulent wings.
The availability of effective shock control technologies is therefore highly desired in connection with future laminar aircraft.
Previous research demonstrated that shock…
UNIVERSITY OF STUTTGART
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THE CHANCELLOR MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE
United Kingdom, Cambridge
Type: University / higher education
Activity type: Higher or Secondary Education Establishments
SME: No
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