In recent years there has emerged a significant increase of interest in the design of Blended Wing Body (BWB) aircraft, specifically applied to a large commercial transport aircraft. The BWB design has been proven to have significant improvements in aerodynamic efficiency, as compared to the conventional wing fuselage design. However, due to inability to counteract significant pitching moments, there is difficulty in the design of high lift devices for BWB, especially trailing edge devices. Due to large wing area increased lift-to-drag ratio, it was found that, in terms of longitudinal stability, high lift devices could be successfully applied to the aircraft, which would meet the take-off and landing requirements for a field length comparable to those of current conventional large transport aircraft.
This is an apporach to design of waveform generator on Virtex-6 FPGA that consume low amount of power. we have worked on different value of using capacitance scaling based thermal aware design waveform generator. There is a reduction of 69.10%, 96.77%, 99.56%, and 99.82% in IOs power as the capacitance is scale down from 50000pF to 5000pF, 500pF, 50pF and 5pF respectively.
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