Research Article
Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing
Table 2
Specifications of test models.
| | Model A | Model B |
| Chord length, c | 80 mm | 40 mm | Thickness, t | 4 mm | 2 mm | Distance between wing elements at leading and trailing edges, G | 40 mm | 20 mm | Distance between wing elements at shoulder, G* | 32 mm | 16 mm | Span, w | 60 mm | 100 mm | Aspect ratio, AR | 0.75 | 2.5 | t/c | 0.05 | 0.05 | G/c | 0.5 | 0.5 |
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