During the first century of flight few major changes have been made to the configuration of subsonic airplanes. A distinct fuselage with wings, a tail, engines and a landing gear persist as the dominant arrangement. During WWII some companies developed tailless all- wing airplanes. The concept failed to advance until 1953 when the British Avro Vulcan bomber appeared. This airplane matched, but did not exceed, the aero performance of it's conventional contemporary, the Boeing B-47. In the late 80's the B-2, became the only flying-wing to have entered major production in recent memory. It proved the benefits of all-wing designs, at least for a stealth platform. The advent of the Blended-Wing-Body addresses the historical shortcomings of all-wing designs, specifically poor volume utility, and excess wetted area as a result. The BWB is now poised to become the new paradigm for large subsonic airplanes. Major aerospace companies are studying the concept for next generation passenger airplanes. But there are still challenges. One is the Blended-Wing- Body's short control lever-arm in pitch. This affects rotation and go-around performance. This paper presents a possible solution by using a novel type of control surface, a belly-flap, on the under side of the wing to enhance its lift- and pitching moment coefficient during landing, go-around and takeoff. Increases of up to 30% in lift-off CL and 8% in positive pitching moment have been achieved during wind tunnel tests on a generic BWB-model with a belly-flap.