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Basics of Fluid Mechanics, 2014a

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8.5. DERIVATIONS OF THE MOMENTUM EQUATION 249<br />

y<br />

a<br />

b<br />

y’<br />

x’<br />

45 ◦<br />

y<br />

a<br />

b<br />

c+b<br />

d+a<br />

c<br />

d<br />

y’<br />

x’<br />

45 ◦<br />

(a) Deformations <strong>of</strong> the isosceles<br />

triangular.<br />

x<br />

(b) Deformation <strong>of</strong> the straight angle<br />

triangle.<br />

x<br />

Fig. -8.11. Different triangles deformation for the calculations <strong>of</strong> the normal stress.<br />

constructed so it equals to dy. The forces acting in the direction <strong>of</strong> x’ on the element<br />

are combination <strong>of</strong> several terms. For example, on the “x” surface (lower surface) and<br />

the “y” (left) surface, the shear stresses are acting in this direction. It can be noticed<br />

that “dx’” surface is √ 2 times larger than dx and dy surfaces. The force balance in the<br />

x’ is<br />

cos θ x<br />

cos θ y<br />

cos θ y<br />

cos θ y<br />

A {}}{<br />

x {}}{ A y {}}{ A y {}}{ A<br />

1 {}}{ 1 {}}{<br />

x {}}{<br />

A x ’<br />

1 {}}{<br />

{ }} {<br />

1<br />

dy τ xx √ + dx τ yy √ + dx τ yx √ + dy τ xy √ = dx √ 2 τ x’x’ (8.73)<br />

2 2 2 2<br />

dividing by dx and after some rearrangements utilizing the identity τ xy = τ yx results in<br />

τ xx + τ yy<br />

+ τ yx = τ x’x’ (8.74)<br />

2<br />

Setting the similar analysis in the y’ results in<br />

τ xx + τ yy<br />

2<br />

− τ yx = τ y’y’ (8.75)<br />

Subtracting (8.75) from (8.74) results in<br />

or dividing by 2 equation (8.76) becomes<br />

2 τ yx = τ x’x’ − τ y’y’ (8.76)<br />

τ yx = 1 2 (τ x’x’ − τ y’y’ ) (8.77)<br />

Equation (8.76) relates the difference between the normal shear stress and the<br />

normal shear stresses in x’, y’ coordinates) and the angular strain rate in the regular (x, y

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