3. The general momentum integral equation can be expressed as, Tw 1 1 U Vw =...

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3. The general momentum integral equation can be expressed as, Tw 1 1 U Vw = (U8*) + PU2 U t + (20+8*) - U U For laminar flow over a non-permeable flat plate with no pressure gradient, the velocity can be approximated by a linear polynomial satisfying the following U, u(0) = 0. Determine the following coefficients boundary conditions u(d) (30%). X == = C Re " * - X == = C2 Rex 0 x = C3 Rex 3. The general momentum integral equation can be expressed as, Tw 1 1 U Vw = (U8*) + PU2 U t + (20+8*) - U U For laminar flow over a non-permeable flat plate with no pressure gradient, the velocity can be approximated by a linear polynomial satisfying the following U, u(0) = 0. Determine the following coefficients boundary conditions u(d) (30%). X == = C Re " * - X == = C2 Rex 0 x = C3 Rex