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2. 2. The flow is steady. In steady (laminar) flow, the velocity of the fluid at each point remains constant. Fluid DYNAMICS Because the motion of real fluids is very complex and not fully understood, we make some simplifying assumptions in our approach. In our model of an ideal fluid, we make the following four assumptions: 1.The fluid is nonviscous. In a nonviscous fluid, internal friction is neglected. Viscous force, Is the resistance that two adjacent layers of fluid have to moving relative to each other

3. 3. The fluid is incompressible. The density of an incompressible fluid is constant. 4. The flow is irrotational. In irrotational flow, the fluid has no angular momentum about any point. STREAMLINES AND THE EQUATION OF CONTINUITY Consider an ideal fluid flowing through a pipe of nonuniform size, as illustrated in Figure Streamline: is the path taken by a fluid particle under steady flow

4. because mass is conserved and because the flow is steady, the mass that crosses A 1 in a time t must equal the mass that crosses A 2 in the time t. That is, m 1 = m 2 or ρ A 1 v 1 t = ρ A 2 v 2 t ; this means that This expression is called the equation of continuity. It states that The product of the area and the fluid speed at all points along the pipe is a constant for an incompressible fluid.

5. BERNOULLI’S EQUATION BERNOULLI’S EQUATION The relationship between fluid speed, pressure, and elevation was first derived in 1738 by the Swiss physicist Daniel Bernoulli. Consider the flow of an ideal fluid through a nonuniform pipe in a time t, as illustrated in Figure. Thus, the net work done by F 1 and F 2 forces are W 1 = F 1 x 1 = P 1 A 1 x 1 = P 1 V. And W 2 = F 2 x 2 = P 2 A 2 x 2 = P 2 V.

6. If m is the mass that enters one end and leaves the other in a time t, then the change in the kinetic energy of this mass is The change in gravitational potential energy is We can apply Equation If we divide each term by V and recall Rearranging terms, we obtain

7. When the fluid is at rest v 1 and v 2 are zero so the Equation becomes This is in agreement with pervious Equation This is Bernoulli’s equation as applied to an ideal fluid. It is often expressed as Bernoulli’s equation Bernoulli’s equation

8. The lift on an aircraft wing can be explained by the Bernoulli effect. Airplane wings are designed so that the air speed above the wing is greater than that below the wing. As a result, the air pressure above the wing is less than the pressure below, and a net upward force on the wing, called lift, results. APPLICATIONS OF BERNOULLI’S EQUATION BERNOULLI’S EQUATIONBERNOULLI’S EQUATION

9. APPLICATIONS OF BERNOULLI’S EQUATION A stream of air passing over one end of an open tube, the other end of which is immersed in a liquid, reduces the pressure above the tube. This reduction in pressure causes the liquid to rise into the air stream. The liquid is then dispersed into a fine spray of droplets. This so-called atomizer is used in perfume bottles and paint sprayers