Final Report - SUPERTRAC (Supersonic transition control)
Project ID: 516100Funded under: FP6-AEROSPACE
This is the final report of the SUPERTRAC project, which aimed to carry out fundamental, numerical and experimental investigations for evaluating the possibilities of laminar flow control on supersonic civil aircraft wings. The report describes the objectives, the background and the structure of the project into specific work packages. It later explains the objectives and the results obtained under each work package and then summarises the overall results and potential impact.
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Record Number: 13130 / Last updated on: 2011-04-14