Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing

Table 1

Specifications of supersonic and transonic wind tunnels of ISAS/JAXA.

	Supersonic wind tunnel	Transonic wind tunnel
Type	Blowdown	Blowdown
Mach number range	1.5–4.0	0.3–1.3
Test section size	600 mm × 600 mm	600 mm × 600 mm
Window size	𝜙 600 mm	𝜙 400 mm
Flow duration	≥30 s	≥30 s
Total pressure	≥149.1 kPa	≥149.1 kPa
Test gas	Dry air	Dry air