Shock-free transonic wing design in combination with supersonic swept wing and area rule concept is the basis for OFW design (Example: 17% thick wing section in flow of Mach = 0.71) |
Pressure signature in the wing plane of optimized OFW (flow of Mach = 1.4 from left to right) |
OFW large transport airplane at the airport (F. Heyl) |
Container concept for loading/unloading an OFW SST |
