1. Fornasier, L., “Treatment of Supersonic Configurations by an Updated Low-Order Method”, J. of Aircraft, Vol. 21, Apr. 1984.
2. Johnson, F.T., “A General Panel Method for the Analysis and Design of Arbitrary Configurations in Incompressible Flows”, NASA CR-3079, 1980.
3. Ehlers, F.E., et al., “A Higher Order Panel Method for Linearized Supersonic Flow”, NASA CR-3062,1979.
4. Fornasier, L., and Heiss, S., “Application of HISSS Panel Code to a Fighter-Aircraft Configuration at Subsonic and Supersonic Speeds”, AIAA Paper 87–2619.
5. Eberle, A., “3-D Euler Calculations Using Characteristic Flux Extrapolation”, AIAA Paper 85–119.