Abstract
It is scientifically important science value and engineering promising to develop the buoyancy-lift integrated hybrid airship for high attitude platform. Through the numerical method, a new tandem wings hybrid airship with both higher utility value and economy efficiency was obtained and its total performance and technical parameters were analyzed in detail. In order to further improve the lift-drag characteristics, we implemented the optimization design for aerodynamic configuration of tandem wings hybrid airship via the response surface method. The results indicate that the tandem wings hybrid airship has considerable volume efficiency and higher aerodynamic characteristics. After optimization, the lift-drag ratio of this hybrid airship was increased by 6.08%. In a given gross lift condition, tandem wings hybrid airship may provide more payload and specific productivity. Furthermore, the size of tandem airship is smaller so the demand for skin flexible materials can be reduced. Results of this study could serve as a new approach to designing buoyancy-lifting integrated hybrid airship.
| Original language | English |
|---|---|
| Pages (from-to) | 1886-1893 |
| Number of pages | 8 |
| Journal | Science China: Physics, Mechanics and Astronomy |
| Volume | 55 |
| Issue number | 10 |
| DOIs | |
| State | Published - Oct 2012 |
Keywords
- Aerodynamic configuration
- Hybrid airship
- Numerical simulation
- Optimization design
- Tandem wings