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The thin shear-layer approximations of the three-dimensional, compressible Navler-Stokes equations are solved for subsonic, transonic, and supersonic flow over axisymmetric boattail bodies at moderate angles of attack. The plume is simulated by a solid body configuration identical to those used in experimental tests. An implicit algorithm of second-order accuracy is used to solve the equations on the ILLIAC IV computer. The turbulence is expressed by an algebraic model applicable todoi:10.2514/3.50980 fatcat:ymqvrbgv5jeplichnpnmdx5rkm