Transitional separation bubbles and unsteady aspects of aerofoil stall

A time-accurate solution method for the coupled potential flow and integral boundary-layer equations is used to study aerofoils near stall, where laboratory experiments have shown high-amplitude low-frequency oscillations. The laminar-turbulent transition model incorporates an absolute instability f...

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Bibliographic Details
Main Author: Sandham, N.D (Author)
Format: Article
Language:English
Published: 2008-07.
Subjects:
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