Vortex structure on twist-morphing micro air vehicle wings.
- Published in:
- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 194, doi. 10.1177/1756829316660321
- By:
- Publication type:
- Article
Works matching IS 17568293 AND DT 2016 AND VI 8 AND IP 3
Results: 5
1
2
Experimental investigation on flow characteristics of a four-wing micro air vehicle.
- Published in:
- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 181, doi. 10.1177/1756829316667770
- By:
- Publication type:
- Article
3
Effect of wing flexibility on flight dynamics stability of flapping wing MAVs in forward flight.
- Published in:
- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 170, doi. 10.1177/1756829316663705
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- Publication type:
- Article
4
Design, development, and flight testing of a high endurance micro quadrotor helicopter.
- Published in:
- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 155, doi. 10.1177/1756829316653694
- By:
- Publication type:
- Article
5
A miniature seven-hole probe air data system and its application on spin prediction.
- Published in:
- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 143, doi. 10.1177/1756829316660320
- By:
- Publication type:
- Article