Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing
Figure 2
Conceptual drawing of boomless supersonic biplane in supersonic level flight [11]. The cross-sectional configuration of the wing is a Busemann-type biplane for sonic boom mitigation. The engines are mounted between the elements; the fuselage is placed on the wing. The cruise Mach number was assumed to be .