Methods of satisfying the stability and control (S&C) requirements for hybrid wing–body (HWB) aircraft are investigated using a multifidelity multidisciplinary optimization framework. A Reynolds-av... Click to show full abstract
Methods of satisfying the stability and control (S&C) requirements for hybrid wing–body (HWB) aircraft are investigated using a multifidelity multidisciplinary optimization framework. A Reynolds-av...
               
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