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A design method for supersonic transport wings
1995
13th Applied Aerodynamics Conference
unpublished
Preserved Fulltext
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