{[ promptMessage ]}

Bookmark it

{[ promptMessage ]}

Airfoil Stall Flow Viz

Airfoil Stall Flow Viz - In the series of pictures shown...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
Flow Over a 2-D Wing Section versus Angle-of-Attack : Recall from our class lecture, a wing generates an increasing amount of lift with increasing angle-of-attack ( ) up to the point when the wing stalls. If we could look at the streamlines we could identify the angle where the streamlines separate from the upper surface of the wing.
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: In the series of pictures shown below, the streamlines are being visualized by injecting a smoke tracer into the wind tunnel flow. In these photos the 2-D wing section stalls at about = 15 degrees. o o o o o...
View Full Document

{[ snackBarMessage ]}