Page 330 - Intro to Tensor Calculus
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               the above equation reduces to the heat equation. Assign units of measurements to each term in the above
               equation and make sure the equation is dimensionally homogeneous.

              I 37. Show that in spherical coordinates the Navier-Stokes equations of motion for a compressible fluid can
               be written
                                   2
                                 V + V  2         ∂p   ∂                       1 ∂        ∂
                           DV ρ   θ    φ                      ∂V ρ        ~                         1 ∂V ρ
                         %(    −         )= %b ρ −   +     2µ ∗   + λ ∇· V   +       µ (ρ   (V θ /ρ)+    )
                                                                     ∗
                                                                                      ∗
                            Dt      ρ             ∂ρ   ∂ρ      ∂ρ              ρ ∂θ      ∂ρ         ρ ∂θ

                                      1   ∂        1  ∂V ρ    ∂
                                 +           µ (          + ρ   (V φ /ρ))
                                               ∗
                                   ρ sin θ ∂φ    ρ sin θ ∂φ  ∂ρ
                                   µ ∗  ∂V ρ  2 ∂V θ  4V ρ    2  ∂V φ   2V θ cot θ      ∂         cot θ ∂V ρ
                                 +    (4    −      −     −           −          + ρ cot θ  (V θ /ρ)+      )
                                    ρ   ∂ρ    ρ ∂θ     ρ    ρ sin θ ∂φ     ρ           ∂ρ           ρ  ∂θ
                                   2
                                 V cot θ         1 ∂p   1 ∂     2µ ∗
                    DV θ   V ρ V θ  φ                             ∂V θ            ~
                                                                              ∗
                  %(     +     −        )= %b θ −    +           (    + V ρ )+ λ ∇· V
                     Dt     ρ       ρ            ρ ∂θ   ρ ∂θ   ρ  ∂θ

                                      1   ∂      sin θ ∂             1   ∂V θ     ∂       ∂          1 ∂V ρ
                                                                                       ∗
                                               ∗
                                 +           µ (        (V φ / sin θ)+      ) +      µ (ρ   (V θ /ρ)+     )
                                   ρ sin θ ∂φ     ρ ∂θ             ρ sin θ ∂φ    ∂ρ       ∂ρ         ρ ∂θ

                                   µ ∗    1 ∂V θ    1   ∂V φ  V θ cot θ          ∂          1 ∂V ρ
                                 +     2        −           −         cot θ +3 ρ   (V θ /ρ)+
                                    ρ     ρ ∂θ    ρ sin θ ∂φ    ρ                ∂ρ         ρ ∂θ

                    DV φ  V φ V ρ  V θ V φ cot θ      1   ∂p    ∂         1  ∂V ρ    ∂
                 %      +      +            = %b φ −         +     µ ∗           + ρ   (V φ /ρ)
                    Dt      ρ        ρ              ρ sin θ ∂φ  ∂ρ     ρ sin θ ∂φ   ∂ρ

                                      1   ∂   2µ ∗  1 ∂V φ
                                                                                  ~
                                                                             ∗
                                 +                         + V ρ + V θ cot θ + λ ∇· V
                                   ρ sin θ ∂φ  ρ   sin θ ∂φ

                                   1 ∂       sin θ ∂              1  ∂V θ
                                 +       µ ∗        (V φ / sin θ)+
                                   ρ ∂θ        ρ ∂θ             ρ sin θ ∂φ

                                   µ ∗      1   ∂V ρ    ∂                  sin θ ∂             1   ∂V θ
                                 +     3            + ρ   (V φ /ρ) +2 cot θ       (V φ / sin θ)+
                                    ρ     ρ sin θ ∂φ   ∂ρ                   ρ ∂θ             ρ sin θ ∂φ
              I 38. Verify all the equations (2.5.28).
              I 39. Use the conservation of energy equation (2.5.47) together with the momentum equation (2.5.25) to
               derive the equation (2.5.48).
              I 40. Verify the equation (2.5.55).
              I 41. Consider nonviscous flow and write the 3 linear momentum equations and the continuity equation
               and make the following assumptions: (i) The density % is constant. (ii) Body forces are zero. (iii) Steady
               state flow only. (iv) Consider only two dimensional flow with non-zero velocity components u = u(x, y)and
               v = v(x, y). Show that there results the system of equations
                                ∂u    ∂u   1 ∂P           ∂v    ∂v   1 ∂P         ∂u   ∂v
                              u    + v   +      =0,     u    + v   +      =0,        +    =0.
                                ∂x    ∂y   % ∂x           ∂x    ∂y   % ∂y         ∂x   ∂y
               Recognize that the last equation in the above set as one of the Cauchy-Riemann equations that f(z)= u−iv
               be an analytic function of a complex variable. Further assume that the fluid flow is irrotational so that
                ∂v   ∂u                              1  2    2     P
                   −    =0. Show that this implies that  u + v  +  = Constant. If in addition u and v are derivable
                ∂x   ∂y                              2           %
               from a potential function φ(x, y), such that u =  ∂φ  and v =  ∂φ , then show that φ is a harmonic function.
                                                           ∂x        ∂y
               By constructing the conjugate harmonic function ψ(x, y) the complex potential F(z)= φ(x, y)+ iψ(x, y)is
                          0
               such that F (z)= u(x, y) − iv(x, y)and F (z) gives the velocity. The family of curves φ(x, y) =constant are
                                                    0
               called equipotential curves and the family of curves ψ(x, y) = constant are called streamlines. Show that
               these families are an orthogonal family of curves.
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