Research Article
The Effect of Rigging Angle on Longitudinal Direction Motion of Parafoil-Type Vehicle: Basic Stability Analysis and Wind Tunnel Test
Table 3
Design parameter of test model and test condition of wind tunnel test.
| | Design parameter of test model | | Parafoil area [m2] | 0.27 | MLL + (ring-shaped part + shackle) [m] | | | Chord length [m] | 0.3 | CG [%] | 45% | | Aspect ratio [-] | 3 | Suspension line material | Vectran | | Mass of parafoil [kg] | 0.2 | Diameter of suspension lines [mm] | 0.47 | | Airfoil section | Clark Y | Number of suspension lines [-] | 12 | | Parameter of test condition | | RA [deg] | 4 to -9 | Dynamic pressure [Pa] | 60, 70, 100,120,150 |
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