1. The flat triangular wing with subsonic leading edges in steady pitch and roll at supersonic velocities;Behrbohm;S.A.A.B. Tech. Note 9,1952
2. Zur Theorie der wenig gestörten homogenen Überschallfelder;Behrbohm,1954
3. Damping in pitch and roll of triangular wings at supersonic speeds;Brown;NACA Rep. 892,1948
4. High-speed Aerodynamics (compressible flow);Carafoli,1959
5. The warping of triangular wings for minimum drag at supersonic speeds;Cohen;J. Aero. Sci.,1957