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Basics of Fluid Mechanics, 2014a

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CHAPTER 10<br />

Inviscid Flow or Potential Flow<br />

10.1 Introduction<br />

The mathematical complication <strong>of</strong> the Naiver–Stokes equations suggests that a simplified<br />

approached can be employed. N–S equations are a second non–linear partial<br />

equations. Hence, the simplest step will be to neglect the second order terms (second<br />

derivative). From a physical point <strong>of</strong> view, the second order term represents the viscosity<br />

effects. The neglection <strong>of</strong> the second order is justified when the coefficient in<br />

front <strong>of</strong> the this term, after non–dimensionalzing, is approaching zero. This coefficient<br />

in front <strong>of</strong> this term is 1/Re where Re is Reynold’s number. A large Reynolds number<br />

means that the coefficient is approaching zero. Reynold’s number represents the<br />

ratio <strong>of</strong> inertia forces to viscous forces. There are regions where the inertia forces are<br />

significantly larger than the viscous flow.<br />

Experimental observations show that when the flow field region is away from a<br />

solid body, the inviscid flow is an appropriate model to approximate the flow. In this<br />

way, the viscosity effects can be viewed as a mechanism in which the information is<br />

transferred from the solid body into depth <strong>of</strong> the flow field. Thus, in a very close<br />

proximity to the solid body, the region must be considered as viscous flow. Additionally,<br />

the flow far away from the body is an inviscid flow. The connection between these<br />

regions was proposed by Prandtl and it is referred as the boundary layer.<br />

The motivations or benefits for such analysis are more than the reduction <strong>of</strong><br />

mathematical complexity. As it was indicated earlier, this analysis provides an adequate<br />

solution for some regions. Furthermore the Potential Flow analysis provides several<br />

concepts that obscured by other effects. These flow patterns or pressure gradients reveal<br />

several “laws” such as Bernoulli’s theorem, vortex/lift etc which will be expanded.<br />

There are several unique concepts which appear in potential flow such as Add Mass,<br />

Add Force, and Add Moment <strong>of</strong> Inertia otherwise they are obscured with inviscid flow.<br />

325

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