1.0. Introduction FLUID MECHANICS 1. INTRODUCTION UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.0. Introduction UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS | ME301 -- FLUID MECHANICS 1.0. Introduction | ME301 -- FLUID MECHANICS UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING 1.0. Introduction 1.1. Solids and fluids Visualization of flow around the F-18 in NASA's water tunnel MATTER Solid Liquid • Strong intermolecular attraction forces • Relative positions of the molecules are fixed • Definite shapes and definite volumes • Medium intermolecular attraction forces • Quite free to change their relative positions • Indefinite shapes but definite volumes Wingtip vortex of an agricultural plain obtained with colored smoke UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS Gas • Very weak intermolecular attraction forces • Practically unrestricted • Indefinite shapes and indefinite volumes FLUIDS UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.2. The concept of continuum 1.2. The concept of continuum Fluids are composed of molecules that are in constant motion and colliding with one another. Can we keep track of each molecule? Fluids are composed of molecules that are in constant motion and colliding with one another. Can we keep track of each molecule? 1m3 of air ~2 × 10 molecules A glass of water ~2 × 10 molecules Statistical approach: ● Equations of motion are written for each separate molecule o Too cumbersome, and even impossible for practical calculations o Intermolecular attraction forces are not known ● Used in statistical mechanics UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1m3 of air ~2 × 10 molecules A glass of water ~2 × 10 molecules Continuum approach: ● Used in most engineering problems ● Principle interest is the gross behavior of the fluid as a continuous material UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.2. The concept of continuum Continuum approach (cont’d): ● Valid whenever the smallest volume of fluid, known as a fluid particle, contains enough number of molecules for making statistical averages. How many is «enough»? Depends on Knudsen Number (Kn) 𝐾𝑛 = 𝜆 molecular mean free path = 𝐿 characteristic linear dimension of the flow field • Molecular mean free path is the average distance travelled by the molecules between two consecutive collisions. • Continuum approach is valid for 𝐾𝑛 < 0.01. • In this course, fluid is treated as continuum. UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.4. The properties of continuum Mass Density, 𝝆 [kg/m3] Domain of continuum P ’ Asymptotic line that defines the density ●Δ𝑚⁄Δ∀ is the average density. ● The average density approaches an asymptotic value as fluid becomes more and more homogeneous. ● When Δ∀ becomes very small, it contains only few molecules and density fluctuates as molecules pass into and out of this volume ● The minimum volume Δ∀′ satisfies the continuum postulate. UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | The description can be made in two ways: a) Material (Lagrangian) Description: An identified fluid particle is followed in the course of time and variation of its properties are described. b) Spatial (Eulerian) Description: Attention is focused on a fixed point in space and variation of fluid properties is observed at that point. UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS Mass Density (cont’d) Domain of molecular effects Continuum hypothesis assumes that, when a fluid particle moves in a flow field, its properties (density, velocity, pressure, temperature…) change i. from point to point ii. from time to time continuously. 1.4. The properties of continuum m/ 1.3. Description of continuum DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS The mass density at point P is given by Δ𝑚 𝜌 = lim ∀→ ∀ Δ∀ ● The density of a fluid is a function of P temperature and pressure. o The density of liquids is slightly affected from these properties so that the density of liquids is almost constant and they are known as incompressible fluids. o The density of gases is strongly affected from these properties so that they are called compressible fluids. UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.4. The properties of continuum 1.4. The properties of continuum Relative Density, s Mass Density (cont’d) 𝑠= For a homogeneous fluid, the average density is 𝑚 𝜌= ∀ The density has units of kg/m3 in SI system of units. UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING The relative density is sometimes referred to as the specific gravity. Specific weight, 𝜸 [N/m3] Force exerted by the gravity field on a unit volume of the fluid, or the weight of the fluid per unit volume. 𝛾 = 𝜌𝑔 𝑔: gravitational acceleration • Not as useful as density since gravitational acceleration changes with location and altitude • Mostly used in hydraulic engineering. • Has units of N/m3 in SI units. | ME301 -- FLUID MECHANICS 1.4. The properties of continuum 𝑉= ∑ 𝑚 𝑉 ∑ 𝑚 | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS No-slip condition ’ The fluid velocity 𝑉(𝑥, 𝑦, 𝑧, 𝑡) at a point 𝑃(𝑥, 𝑦, 𝑧) is defined as the instantaneous velocity of the center of gravity of the volume UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION 1.4. The properties of continuum z Fluid velocity, 𝑽 [m/s] Density of any substance 𝜌 = Density of water 𝜌 𝑉(𝑥, 𝑦, 𝑧, 𝑡) 𝑃 r y It is an experimental fact that the fluid particles which are in direct contact with the solid boundary, has the same velocity as the boundary itself. In other words, the fluid sticks to the solid boundaries. x 𝑁 : number of molecules inside 𝑚 : mass of the 𝑖 th molecule 𝑉 : volume of the 𝑖 th molecule UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.4. The properties of continuum Couette flow ℎ 𝑦 𝑈 𝑈 𝑢(𝑦) 1.4. The properties of continuum Forces Acting on a Body of Fluid, 𝑭 [N = kg m/s2] 𝑈 𝑢= 𝑦 ℎ 𝑣=0 𝑤=0 Body forces ● Distributed over the entire volume of fluid. 𝑥 𝑢=0 Hagen-Poiseuille flow ● Defined as the force per unit mass of the fluid 𝑢=0 𝑟 𝑅 𝑧 𝑉 𝑟 𝑉 =0 𝑉 =0 𝑟 1− 𝑅 𝑉 =𝑉 𝑢=0 UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.4. The properties of continuum Δ𝐴 𝑃 Δ𝐹 Δ𝐹 𝐹 ● Gravitational force per unit mass: gravitational acceleration, 𝑔⃗ UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS Stress field at a point is a tensor quantity. 𝜏 ◦ Nine components 𝜏 Cartesian stress tensor: 𝜎 𝜏 𝜏 𝜏 𝜎 𝜏 𝜏 𝜏 𝜎 lim → dirn. of surface normal | 𝑃 𝐹 𝑦 → UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION 𝑛 𝐹 :normal force 𝐹 : tangential (shear) force lim Shear stress, 𝜏, at point P 𝜏= 𝑃 Stress (cont’d) 𝑛 Δ𝐹⃗ Normal stress, 𝜎, at point P 𝐹⃗ 𝐹⃗ ● Caused by gravitational fields, magnetic field and electrostatic fields 1.4. The properties of continuum Stress, 𝝈, 𝝉 [Pa = N/m2] 𝜎= Surface forces ● Forces exerted on the boundaries of a fluid element by its surroundings via direct contact at the surface. DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 𝜎 𝑥 𝑧 dirn. of force UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 1.4. The properties of continuum 1.4. The properties of continuum Pressure [Pa = N/m2] Pressure (cont’d) 𝑧 ● Is the normal component of a force acting on an area divided by that area. 𝑧 𝑝 𝐴 𝑛 ● Has the same magnitude as the 𝑝 𝐴 normal stress, but it acts in a direction opposite to the unit normal vector of this area. ● Pressure at a point is independent of direction, whenever the fluid is at rest. 𝑝 𝐴 𝑝 𝐴 cos 𝛼 𝑘 𝑗 𝑖 𝑥 𝑦 𝑦 ● The prism is small enough so that the pressure on each face may be assumed constant. ● For a fluid at rest, sum of the forces acting on the body of fluid must be equal to zero. 𝑧 𝑝 𝐴 𝑛 𝑝 𝐴 𝑝 𝐴 cos 𝛼 𝑗 𝑖 𝑥 𝑦 𝑦 𝑝 𝐴 𝑥 or in scalar form 𝑝 𝐴 𝑘 𝐹⃗ = 0 𝑝 𝐴 𝑥 𝑧 ∑ 𝐹 = 0, ∑ 𝐹 = 0, ∑ 𝐹 = 0 UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION 1.4. The properties of continuum Pressure (cont’d) ∀ of the prism 𝐹 = 𝑝 𝐴 − 𝑝 𝐴 cos 𝛼 + 𝑓 𝐴 𝑦 3 body force in 𝑦-dirn Pressure (cont’d) 𝑧 𝑧 𝜌=0 𝑝 𝐴 𝑛 𝑝 𝐴 𝐴 : area of the prism in the 𝑥𝑧 plane 𝑥 𝑝 : average pressure on the area 𝐴 𝑥 𝐴 : area of the inclined surface 𝑝 : average pressure on the area 𝐴 𝛼: angle between the normals of the surfaces 𝐴 and 𝐴 𝑦 : intercept of the prism faces on the 𝑦-axis | | ME301 -- FLUID MECHANICS 𝑝 𝐴 cos 𝛼 𝑗 DEPARTMENT OF AERONAUTICAL ENGINEERING 𝑦 𝑦 ME301 -- FLUID MECHANICS 𝑧 𝜌=0 𝑓 𝜌𝑦 3 𝑝 𝐴 𝑛 𝑝 𝐴 𝐴 = 𝐴 cos 𝛼 𝐴 = 𝑝 −𝑝 + | 𝐴 𝑦 3 From the geometry of the prism: 𝐴 𝑦 𝑝 𝐴 −𝑝 𝐴 +𝑓 𝜌 3 𝑝 𝐴 𝑧 𝐹 = 𝑝 𝐴 − 𝑝 𝐴 cos 𝛼 + 𝑓 𝑝 𝐴 𝑘 𝑖 UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION DEPARTMENT OF AERONAUTICAL ENGINEERING 1.4. The properties of continuum mass inside the prism ● Hence, in 𝑦-dirn: | 𝑝 𝐴 𝑝 𝐴 cos 𝛼 𝑘 𝑗 𝑖 =0 𝑥 𝑥 𝑦 𝑝 𝐴 =0 UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 𝑦 1.4. The properties of continuum Pressure (cont’d) 𝑝 −𝑝 + 𝑓 𝜌𝑦 3 𝑧 𝑧 =0 As 𝑦 → 0, in the limit, eqn. becomes 𝑝 =𝑝 𝑛 𝑝 𝐴 𝑥 ∑𝐹 = 0 𝑝 = 𝑝 𝑥 Hence, 𝑝 =𝑝 =𝑝 =𝑝 =𝑝 𝑝 𝐴 cos 𝛼 𝑗 𝑖 ∑𝐹 = 0 𝑝 = 𝑝 𝑝 𝐴 𝑘 Similarly; UNIVERSITY OF TURKISH AERONAUTICAL ASSOCIATION 𝑝 𝐴 𝑦 𝑝 𝐴 the pressure at a point is equal in all directions for a fluid at rest | DEPARTMENT OF AERONAUTICAL ENGINEERING | ME301 -- FLUID MECHANICS 𝑦