A-to-Z Guide to Thermodynamics,
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Visualization of the boundary layer transition in low-speed flow

This movie presents a full set of images from a wind tunnel test combined in an animation. In the test, the 65° delta wing model of 420 mm length and 332 mm span was tested in subsonic wind tunnel at constant flow speed of 50 m/s and varying the angle of attack

Read more in Visualization of boundary layer transition by viscous oil

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