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| V-22 3-D model mounted above rotors |
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| XV-15 3-D model waiting for testing |
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| XV-15 3-D test wing with flaps and accuators. |
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| XV-15 test rotors. |
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| XV-15 rotor mounted in 3-D testing area |
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| 70 degree delta wing with LE AFC mounted in water tunnel |
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| Model of XV-15 wing for 2-D testing |
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| Open loop windtunnel testing ellipse with leading and trailing edge blowing |
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| Close up of ellipse during testing |
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| Modified NACA 0012 with divergent trailing edge and active flow control |
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| Coanda cylinder. This experiment does not include free stream blowing, only slot blowing |
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| Modified GLASII. Control of seperation via slot blowing yeilds a highly efficient airfoil |
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