The acoustics of simplified engine over-the-wing configurations, with and without jet flow attachment to the shielding surface were studied at model scale. The nozzle used consisted of a 5:1 slot nozzle (equivalent diameter, 5.1 cm) operated at a jet Mach number of 0.6, with the flow directed at angles of 0° to 10° to the shielding surface (flat board). The shielding length of the surface was varied from 16.4 to 54.3 cm, and the nozzle height above the surface was varied from 0 to 7.6 cm. Also, the velocity field at the trailing edge of each nozzle/surface configuration was mapped. With attached flow, the jet flow field is stretched in the flow direction, resulting in locally higher velocities than those for unattached flow or nozzle only. This increased the noise levels for the attached flow cases compared to those with partially or completely unattached flow. With attached flow, the shielding benefits were substantially reduced (up to half) compared with fully detached flow. Increasing the impingement angle of the jet flow from 0° to 10° generally caused the noise levels to increase. In some cases, the noise increase was sufficiently broad-band that the jet noise shielding benefits were noticeably reduced.