A wind tunnel test was conducted to obtain pressure and flow visualization data from geometrically simple wing and store shapes under mutual interference conditions with the store both at its carriage position and selected points along a realistic store separation trajectory. The test was conducted at nominal Mach numbers of 0.95 and 1.2 at a nominal Reynolds number of 2.4 million/ft. Data were acquired for wing and store angles of attack of 0, 2, and 6 deg.