An Oblique Flying Wings (OFW) was simulated to analyze the aerodynamic performance and started to design using an inverse problem solver. An OFW is a wing of elliptic planform having minimum wave drag at transonic and supersonic speeds up to M=1.4. In our simulation, the maximum lift to drag ratio (L/D) was 20.44 at Mach 1.414 and angle of attack 0.75. In this case, a shock wave did not appear …

