Numerical simulations of the wing wake and tip vortex for air-to-air refuelling
The present research was carried out in the framework of the ASTRAEA II project, in collaboration with Cobham Mission Equipment. One part of the overall ASTRAEA II project is to design an autonomous air-refuelling system based on a wake model computed in real-time, which allows the flow field to be...
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Cranfield University
2016
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/10236 |