- Reynolds transport theorem
**Reynolds transport theorem**is a fundamental theorem used in formulating the basic conservation laws offluid dynamics . These conservation laws (law of conservation of mass , law of conservation of linear momentum, and law of conservation of energy) are adopted fromclassical mechanics andthermodynamics where the system approach is normally followed. In fluid mechanics, it is often more convenient to work withcontrol volume s as it is difficult to identify and follow a system of fluid particles. Thus, there is a need to relate the system equations and corresponding control volume equations. The link between the two is given by the Reynolds Transport Theorem.Imagine a system and a coinciding control volume with a control surface. Reynolds transport theorem states that the

rate of change of anextensive property N, for the system is equal to the time rate of change of N within the control volumeand the net rate of flux of the property N through the control surface. For an example, the law of conservation of mass states that rate of change of the property, mass, is equal to the sum of the rate of accumulation of mass within a control volume and the net rate of flow of mass across the control surface.The differential forms of these equations with additional assumptions are commonly known as the

Navier-Stokes equations . The additional assumptions are the Newton's viscosity law and the Fourier's conduction law.**General Form**The Reynolds transport theorem refers to any extensive property, N, of the fluid in a particular

control volume . It is expressed in terms of asubstantive derivative on the left-hand side.$frac\{DN\_\{sys\{Dt\}\; =\; int\_\{c.v.\}^\{\}\; frac\{partial\}\{partial\; t\}\; (\; ho\; eta)\; dV\; +\; int\_\{c.s.\}^\{\}\; ho\; eta\; vecupsilon\_bcdot\; widehat\{n\}\; dA+int\_\{c.s.\}^\{\}\; ho\; eta\; vecupsilon\_rcdot\; widehat\{n\}\; dA$,

where η is the intensive property related to extensive property N, (N per unit mass), t is time, c.v. refers to the control volume, c.s. refers to the control surface, ρ is the fluid density, V is the volume, $upsilon\_b$ is the velocity of the boundary of the control volume (the control surface), $upsilon\_r$ is the velocity of the fluid with respect to the control surface, n is the outward pointing normal vector on the control surface, and A is the area.

**Mass Formulation**Also called the continuity equation, the control volume form of the conservation of mass is found by substituting mass in for N. This means that η is equal to 1.

$0=;int\_\{c.v.\}^\{\}frac\{partial\; ho\}\{partial\; t\}\; dV\; +\; int\_\{c.s.\}^\{\}\; ho\; vec\{v\}\_b\; cdot\; widehat\{n\};dA\; +\; int\_\{c.s.\}^\{\}\; ho\; vec\{v\}\_r\; cdot\; widehat\{n\};dA$

All variables are defined as in the general formulation. M is equal to the mass of the control volume. Applying the

Conservation of mass principle, the left hand side reduces to 0 since mass of a system cannot change in time. In a steady flow system, the first term on the right hand side of the equation will be equal to 0, i.e. the mass of the control volume does not change, implying that the mass flow rate into the control volume is equal to the mass flow rate out of the control volume.**Momentum Formulation**The momentum equation is found by substituting momentum in for N. From this, η is found to be velocity. From Newton's second law, we have the time rate of change of momentum (now the left hand side of the equation) is equal to the net force. Thus,

$sum\_\{\}\; vec\{F\}=int\_\{c.v.\}^\{\}frac\{partial\}\{partial\; t\}(\; ho\; vecupsilon)\; dV\; +\; int\_\{c.s.\}^\{\}\; ho\; vecupsilon(vecupsilon\_b\; cdot\; widehat\{n\})dA\; +\; int\_\{c.s.\}^\{\}\; ho\; vecupsilon(vecupsilon\_r\; cdot\; widehat\{n\})dA$,

where F is force, $upsilon$ is the velocity of fluid in a coordinate system attached to the control surface, and all other variables are defined as in the general formulation. Note that the integral form of the momentum equation is a vector equation.

**Energy Formulation**The energy equation is found by substituting energy in for N. From this, η is found to be energy per unit mass.

$dot\{Q\}-sum\{\}\; dot\{W\}=int\_\{c.v.\}^\{\}\; frac\{partial\}\{partial\; t\}\; left\; [\; ho\; left\; (\; frac\{upsilon^2\}\{2\}+gz+\; ilde\{u\}\; ight\; )\; ight\; ]\; dV\; +\; int\_\{c.s.\}^\{\}\; left\; [frac\{upsilon^2\}\{2\}+gz+\; ilde\{u\}+frac\{p\}\{\; ho\}\; ight]\; ho\; vecupsilon\_bcdotwidehat\{n\}dA\; +\; int\_\{c.s.\}^\{\}\; left\; [frac\{upsilon^2\}\{2\}+gz+\; ilde\{u\}+frac\{p\}\{\; ho\}\; ight]\; ho\; vecupsilon\_rcdotwidehat\{n\}dA$

where Q is the heat transfer into the control volume, W is the work done by the system, g is the acceleration due to gravity, z is the vertical distance from an arbitrary datum, $ilde\{u\}$ is the specific

internal energy of the fluid, p is the pressure and all other variables are defined as in the general formulation.Note that these equations make no consideration for chemical reactions or potential energy associated with

electromagnetic field s.**See also***

Navier-Stokes equations

*Reynolds number **References*** M.C. Potter, J.F. Foss, "Fluid Mechanics", Great Lakes Press, 1982

* http://www.catea.org/grade/mecheng/mod6/mod6.html#slide1

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