Works matching IS 17568293 AND DT 2018 AND VI 10 AND IP 1
Results: 8
Reduced-order methodology for prediction of loads generated by a flexible flapping wing.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 31, doi. 10.1177/1756829317708318
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- Article
Investigation into Reynolds number effects on a biomimetic flapping wing.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 106, doi. 10.1177/1756829317745319
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- Article
Experimental maneuverability and agility quantification for rotary unmanned aerial vehicle.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 3, doi. 10.1177/1756829317736204
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- Article
Dove: A biomimetic flapping-wing micro air vehicle.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 70, doi. 10.1177/1756829317734837
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- Article
Characterizing and modeling the enhancement of lift and payload capacity resulting from thrust augmentation in a propeller-assisted flapping wing air vehicle.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 50, doi. 10.1177/1756829317734836
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- Article
Attitude controller optimization of four-rotor unmanned air vehicle.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 42, doi. 10.1177/1756829317734835
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- Article
Reduction of the head-up pitching moment of small quad-rotor unmanned aerial vehicles in uniform flow.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 85, doi. 10.1177/1756829317745318
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- Article
Aerodynamic comparisons of flexible membrane micro air vehicle wings with cambered and flat frames.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 12, doi. 10.1177/1756829317705327
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- Article