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Problems in Mathematical Analysis.pdf - pwp.net.ipl.pt

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Sec. 6]_Applications of the Double Integral <strong>in</strong> Mechanics_261<br />

moments M x and M Y relative to the x- and t/-axes are expressed by the<br />

double <strong>in</strong>tegrals<br />

A4 --=<br />

H jj<br />

Q (x, y) dx dy, M x =<br />

J<br />

yQ (x,<br />

J<br />

y) dx dy,<br />

(S) (S)<br />

M Y =^ y)dxdy.<br />

J*e(x,<br />

(1)<br />

(5)<br />

If the lam<strong>in</strong>a is homogeneous, then Q (x, y) const.<br />

2. The coord<strong>in</strong>ates of the centre of gravity of a lam<strong>in</strong>a. If C (x, y) is the<br />

centre of gravity of a lam<strong>in</strong>a, then<br />

- My -M x<br />

y _i_ / / . _d<br />

' J ~ ' M M<br />

where M is the mass of the lam<strong>in</strong>a and M x , My are its static moments relative<br />

to the coord<strong>in</strong>ate axes (see 1). If the lam<strong>in</strong>a is homogeneous, then <strong>in</strong><br />

formulas (1) we can put Q=l.<br />

3. The moments of <strong>in</strong>ertia of a lam<strong>in</strong>a. The moments of <strong>in</strong>ertia 01 a<br />

lam<strong>in</strong>a relative to the x- and t/-axes are, respectively, equal to<br />

/X= S<br />

y'Q (x,<br />

S<br />

y) dx dy, /r= J J<br />

(S) (S)<br />

The moment of <strong>in</strong>ertia of a lam<strong>in</strong>a relative to the orig<strong>in</strong> is<br />

* 2<br />

Q (*. y) *x dy. (2)<br />

Putt<strong>in</strong>g Q(X, //)-=! <strong>in</strong> formulas (2) and (3), we get the geometric moments of<br />

<strong>in</strong>ertia of a plane iigure.<br />

2225. F<strong>in</strong>d the mass of a circular lam<strong>in</strong>a of radius R if the<br />

density is proportional to the distance of a po<strong>in</strong>t from the centre<br />

and is equal to 6 at the edge of the lam<strong>in</strong>a.<br />

2226. A lam<strong>in</strong>a has the shape of a right triangle with legs<br />

OB = a and OA = b, and its density at any po<strong>in</strong>t is equal to the<br />

distance of the po<strong>in</strong>t from the leg 0/4. F<strong>in</strong>d the static moments<br />

of the lam<strong>in</strong>a relative to the legs 0/4 and OB.<br />

2227. Compute the coord<strong>in</strong>ates of the centre of gravity of the<br />

area OmAnO (Fig. 96), which is bounded by the curve // s<strong>in</strong>*<br />

and the straight l<strong>in</strong>e OA that passes through the coord<strong>in</strong>ate orig<strong>in</strong><br />

and the vertex A (-^ ,<br />

Ij<br />

of a s<strong>in</strong>e curve.<br />

2228. F<strong>in</strong>d the coord<strong>in</strong>ates of the centre of gravity of an area<br />

bounded by the cardioid r = a(\ + cosij)).<br />

2229. F<strong>in</strong>d the coord<strong>in</strong>ates of the centre of gravity of a circular<br />

sector of radius a with angle at the vertex 2a (Fig. 97).<br />

2230. Compute the coord<strong>in</strong>ates of the centre of gravity of an<br />

area bounded by the parabolas // = 4.x f 4 and if = 2x4-4.<br />

2231. Compute the moment of <strong>in</strong>ertia of a triangle bounded<br />

by the straight l<strong>in</strong>es x + y 2, # = 2, y = 2 relative to the #-axis.<br />

(3)

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