Blockage-tolerant wind tunnel measurements for a NACA 0012 at high angles of attack
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文摘

Existing post-stall data is demonstrated to be too inaccurate for VAWT analysis.

Two NACA-0012 aerofoils are tested through 180° of incidence.

A blockage tolerant and a conventional wind tunnel test section are used.

Conventional tunnel data requires blockage corrections unsuited to extensively separated flow.

The tolerant tunnel raw data does not need corrections.

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