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|Title:||Separated flow around an airfoil with a spoiler||Authors:||Xu, Cheng.||Keywords:||DRNTU::Engineering::Aeronautical engineering::Aerodynamics||Issue Date:||1997||Abstract:||When a spoiler is erected rapidly on the upper surface of a wing, it brings about a long-term reduction in lift and an increase in drag. However, it has a transient effect of increasing the lift (usually referred to as the adverse lift) on the wing due to the creation of a starting vortex shed from the tip and convected downstream of the spoiler. This thesis is devoted to a numerical study of the unsteady separated flow around an airfoil with a spoiler.||URI:||http://hdl.handle.net/10356/19974||Rights:||NANYANG TECHNOLOGICAL UNIVERSITY||Fulltext Permission:||restricted||Fulltext Availability:||With Fulltext|
|Appears in Collections:||MAE Theses|
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