An Experimental Investigation Of Incompressible Flow Over Delta And Double Delta Wings
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An Experimental Investigation of Incompressible Flow Over Delta and Double-Delta Wings
| Author | : James K. Nathman |
| Publisher | : |
| Total Pages | : 79 |
| Release | : 1976 |
| Genre | : |
| ISBN | : |
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An experimental study of the flow over delta and double-delta wings was conducted in a 7' x 10' low speed wing tunnel. The configurations tested were AR-3 and AR-4 delta wings and the AR-4 wing which was modified with AR-1 and AR-2 strakes attached to form double-delta wings. Pressure measurements, surface flow visualization, and vortex core visualization studies were conducted over a wide range of angles of attack.
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