A design method for supersonic transport wings

Pei Li, Helmut Sobieczky, Richard Seebass
1995 13th Applied Aerodynamics Conference   unpublished
We report here results from our use of the fictitious gas method for the design of supersonic transport wings using the Euler equations. While the example chosen here is the oblique flying wing, the technique has general application to supersonic wings with subsonic leading edges.
doi:10.2514/6.1995-1819 fatcat:s5qcjhoscjh53oy6ah74usg22y