A numerical study of performance of the small-size uav pushing tandem propeller with joined blades
A new shape of the tandem blade with an improved arrangement of profiles, in relation to the known propellers, in which the profiles are located similar to those in the tandem wing of an airplane is developed. A new arrangement of profiles along the height of the blade is proposed. The basis for the...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
PC Technology Center
2020-04-01
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| Series: | Eastern-European Journal of Enterprise Technologies |
| Subjects: | |
| Online Access: | http://journals.uran.ua/eejet/article/view/199486 |