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