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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Format: | Article |
Language: | English |
Published: |
2008-07.
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Online Access: | Get fulltext |