Research Article
The Effect of Rigging Angle on Longitudinal Direction Motion of Parafoil-Type Vehicle: Basic Stability Analysis and Wind Tunnel Test
Table 2
Design parameters and mainstream conditions.
| Design parameter | Chord length [m] | 0.30 | Wing area [m2] | 0.90 | Aerodynamic center [%] | 25 | [%] | 45 | [m] | 0.62 | Mass [kg] | 0.2 | Airflow condition | Dynamic pressure [Pa] | 150 |
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