[KongchangAI]
Unverified50% confidenceFactExact time

The stall angle of attack was predicted to be 7 degrees, consistent with the wind tunnel, but the maximum lift is lower than the wind tunnel result because the SST model cannot simulate the sudden stall in the wind tunnel.

1
Sources
50%
Confidence
Long-term
Relevance
10/24/2026
First Seen

Sources

Hands-On with a Research Simulation Agent: One Prompt Runs a Full NASA Airfoil Validation

Related Entities

k-omega SSTconceptNACA 0012concept

Related Claims

UnverifiedIn the result comparison, the suction peak at 10 degrees angle of attack differs from wind tunnel/CFL3D data by only 0.2%, the lift curve slope differs by 0.8%, and the stall angle of attack of 7 degrees matches the wind tunnel, but the maximum lift coefficient is low.72% similar

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