Report copyright - Adaptive Shock Control Bumps - Imperial College … p 0 = 1 y d P 0 1 R y d 0 P 1 + 1 2 M 2) 1 dy (1) minfC p 0 g (2) s.t. ˙ max (1 k)˙ y (3) In which C p 0 is total pressure coe
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