Reynolds number effects on flow topology above blunt-edge delta wing VFE-2 configurations

This paper discusses further the effects of Reynolds number, angle of attack and leading edge bluntness on the flow topology above delta wing VFE-2 configurations. In this project two delta wing models differentiated by its leading edge radius to the mean aerodynamics chord ratio of 0.15 and 0.3, na...

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Bibliographic Details
Main Authors: Said, Mazuriah, Mat, Shabudin, Mansor, Shuhaimi, Abdul Latif, Ainullotfi, Mat Lazim, Tholudin
Format: Conference or Workshop Item
Published: 2015
Subjects:
Online Access:http://eprints.utm.my/id/eprint/60586/
https://pure.utm.my/en/publications/reynolds-number-effects-on-flow-topology-above-blunt-edge-delta-w
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