Oblique Flying Wing Supersonic Transport

Aerodynamic optimization and concept for future air transport or unmanned aerial vehicle (UAV)

 

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

 

2008