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    Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow

    Shock control bumps are a means to reduce wave drag that occurs at the upper limit of civil transport aircrafts flight envelope. An SCB was optimized for and applied to the rigid wing-body DLR F11 model. The e...

    Benedikt König, Martin Pätzold… in New Results in Numerical and Experimental … (2008)