1. Obsborn, R. F. and Gallaway, C. R. Wing-In-Ground Effect Technology Workshop Proceedings, AFWAL/FIMM, September 1978. Goetz, A. R., Osborn, R. F., and Smith, M. L., wWing-In-Ground Effect Aerodynamic Predictions Using PANAIR," AIAA Paper 84-2429, 1984. Gallington, R. W., Miller, M. K., and Smith, W. D."The Ram-Wing Surface Effect Vehicle: Comparison of One-Dimensional Theory with Wind Tunnel and Free Flight Results," SRL-TR-71-0012, July 1971. Agarwal, R. K. and Deese, J. E."Numerical Solutions of the Euler Equations f o r Flow Past an Airfoil i n Ground Effect," AIAA Paper 84-0051 , 1984. Brown, J. R."Wind Tunnel Investigation of Single and Tandem Low Aspect Ratio Wings i n Ground Effect .11 TRECOM TR-63-63, March 1964. Agarwal, R. K. and Deese, J. E."Transonic Wing-Body Calculations Using Euler Equations," AIAA Paper 83-1853, 1983. Jameson, A., Schmidt, W., and Turkel, E."Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping scheme^,^^ AIAA Paper 81-1259, 1981. Jameson, A. and Baker, T. J. "Solution of the Euler Equations for Complex Configurations ,'I AIAA Paper 83-1929, 1983. Eiseman, P. R. "A Multisurface Method of Coordinate Generation," J. Comp. Phys., Vol.33, 1979. pp.118-150. Jacobs, E. N. and Anderson, R. F."Large Scale Aerodynamic Characteristics of Airfoils as Tested i n the Variable Density Wind Tunnels," NACA TN 352, 1930. Figure 10. Variation of lift coefficient CLwith h/& for a wing in