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For an incompressible boundary layer flow over a flat plate shown in the figure, the momentum thickness is expressed as

  1. $\int_0^{\infty} \frac{u}{U_{\infty}} d y$
  2. $\int_0^{\infty}\left(1-\frac{u}{U_{\infty}}\right) d y$
  3. $\int_0^{\infty} \frac{u}{U_{\infty}}\left(1-\frac{u}{U_{\infty}}\right) d y$
  4. $\int_0^{\infty}\left(1-\frac{u^2}{U_{\infty}^2}\right) d y$

 

 

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