... ⌠ ⎮ 2 m = ⎮ ρ π b ⎜1 − ⎜ ⎮ ⎝ ⌡0 a 2 ⎟ dx = a ρ π b2 a ⎠ x ρ = 2 ⌠ ⎮ ⎛ 3m ⎞ ⎛ Ix = ⎮ π b ⎜1 − ⎜ 2 ⎜ ⎮ ⎝ 2 a b ⎠ ⎝ ⌡0 22 ⎟ b2 ⎛1 − x ⎟ dx = m b2 ⎜ 2 ⎜ 2 a ⎠ ⎝ a ⎠ x 3m 2 a b Ix = 2 mb ... Given: b = in t = in Solution: ⎡1 I x = 2 ⎣ 12 Ix = 55.55 in ⎡1 I y = 2 ⎣ 12 ⎛ ⎝ a t + a t ⎜b − t⎞ ⎟ 22 ⎥ + t ( 2b − 2t) ⎦ 12 ⎛ a − t + t ⎞ ⎤ + 2b t3 ⎟⎥ ⎠ ⎦ 12 ⎝ t ( a − t) + t( a − t) ⎜ ⎡a − t ... ( a + b) c + 2b d + 2b d ⎜ ⎟ 12 ⎝ 2 Iy = 4 Ix = 5.515 × 10 in 1 3 [ 2( a + b) ] c + ( 2b) d 12 12 Iy = 1.419 × 10 in Ixy = in Iu = Ix + Iy Ix − Iy + cos ( 2 ) − Ixy sin ( 2 ) 2 Iu = 3.47 ×...
... = 25 mm b = 25 0 mm c = 50 mm d = 150 mm Solutuion: ⎛ b ⎞ b2a + ⎛ b + ⎜ ⎟ ⎜ ⎝ 2 ⎝ yc = c⎞ ⎟ 2d c 2 b2a + c2d yc = 20 7 mm b⎞ 3 ⎞ ⎛ ⎛ c Ix' = 2a b + 2a b ⎜ yc − ⎟ + 2d c + c2d ⎜ b + − yc⎟ 12 2⎠ ... the publisher Engineering Mechanics - Statics Chapter 10 Solution: 2a b yc = Ix = b ⎛ c⎞ + 2c b⎜ b + ⎟ ⎝ 2 yc = 12. 50 mm 2a b + 2c b 12 2a b + 2a b ⎛ yc − ⎜ ⎝ b⎞ ⎟ 2 ⎡1 + 2 ⎣ 12 b c + b c ⎛b ... publisher Engineering Mechanics - Statics Chapter 10 Given: a = 150 mm b = 20 0 mm t = 20 mm θ = 20 deg Solution: Moments of inertia Ix and Iy: Ix = 1 3 2a ( 2b) − ( 2a − t) ( 2b − 2t) 12 12 Ix =...
... = 50 mm d2 = 35 mm h = 110 mm t = 15 mm Solution: 2 ⎛ d1 ⎞ d1 ⎛ d + h ⎞ + π ⎛ d2 ⎞ ⎛ d + h + d2 ⎞ π⎜ ⎟ + h t⎜ ⎜ ⎟ ⎜ ⎟ ⎟ 222 ⎝ 2 ⎝ yc = 2 ⎛ d1 ⎞ ⎛ d2 ⎞ π ⎜ ⎟ + ht + π ⎜ ⎟ 22 yc = 85.9 ... publisher Engineering Mechanics - Statics Chapter d = in e = in f = in Solution: zc = ⎛ a⎞ ⎟ + 2( d − e)a⎜ ⎟ ⎝ 2 ⎝ 3⎠ ( 2e f a) + 2e a⎛ ⎜ 2d b + a⎞ ( 2c b) + zc = 1. 625 in 2d( a + f) Problem 9- 82 Each ... publisher Engineering Mechanics - Statics Chapter Given: a = 300 mm b = 400 mm Solution: L = πa 2+2 a +b xc = 1⎡ π a ⎛ 2a ⎞⎤ 2a ⎢ a + b + ⎜ ⎟⎥ L⎣ 2 ⎝ π ⎠⎦ yc = 1⎡ π a ⎛ 2a ⎞⎤ 2a ⎢ a + b + ⎜ ⎟⎥ L⎣ 2...
... z dy Solution: b ⌠ ⎮ 2 V = ⎮ π a ⎜1 − ⎜ ⎮ ⎝ ⌡0 z =a 2 ⎜ ⎜ ⎝ 2 y 1− b ⎟ 2 ⎠ 22 ⎟ d y = b b − b a2 π 2 b ⎠ b y b ⌠ ⎮ 2 ⎜ yc = ⎮ yπ a − ⎜ 2b a π ⎮ ⎝ ⌡0 2 ⎟ d y = b2 2 8b b ⎠ y By symmetry ... the publisher Engineering Mechanics - Statics Chapter Solution: a ⌠ A=⎮ ⌡0 ( 2) 2 a a y dy = a ⌠ ⎮ xc = 2 2a ⌡ 2a A= a xc = a yc = a y dy = a a 5 a yc = ( ) ⌠ ⎮ y a y dy = a 2 2a 5a Problem ... writing from the publisher Engineering Mechanics - Statics Chapter Solution: 2 x +y =a y= 2 a −x a A = π xc = A W = Aγ W = 62. 8 32 lb a ⌠ ⎮ x a2 − x2 dx ⌡0 ⌠ ⎮ yc = A⎮ ⌡ a ( ) 2 a − x dx xc = 1.698...
... Engineering Mechanics - Statics ⌠ ⎮ P= ⎮ ⌡ 2 R2 ⌠ ⎮ ⎮ ⌡R Chapter ⎛ R2 ⎞ ⎟ r dr dθ ⎝ r ⎠ p0 ⎜ P = 2 p0 R2 ( R − R ) p0 = P 2 R ( R − R ) 2 ⌠ ⌠ M = ⎮ r dF = ⎮ ⌡ ⌡ A ⌠ ⎮ M= ⎮ ⌡ 2 ⌠ ⎮ ⎮ ⌡ 2 ... writing from the publisher Engineering Mechanics - Statics Chapter ⎛d − c ⎟ ⎞ M2 = μ s P' ⎜ ⎜ d2 − c2 ⎟ ⎝ ⎠ P' = P' b − P a = P = P' 3M2 ⎛ d2 − c2 ⎞ ⎜ ⎟ P' = 88.5 N 2 s ⎜ d3 − c3 ⎟ ⎝ ⎠ ⎛ b⎞ ⎜ ... M= ⎮ ⌡ 2 ⌠ ⎮ ⎮ ⌡ 2 R2 ⌠ ⎮ ⌡R rμ s p0 r dr dθ ( ⎛ R2 ⎞ 2 ⎟ r dr dθ = π μ s p0 R R − R r ⎠ ⎝ μ s p0 ⎜ ) ( P 2 ⎤ ⎡ M = π μ s⎢ ⎥ R2 R2 − R1 2 R2( R2 − R1 )⎦ ) M= μ s P(R2 + R1) Problem 8-118...
... −P c + 2 b +c Fmax c = F max b P = 2 P = 28 2.843 N b +c c B z + Dz − Fmax b +c F max c Bz = 2 =0 Dz = B z b +c Dz = Bz B z = 28 3 N Dz = 28 3 N b B y + Dy − Fmax b +c F max b By = 2 =0 2 b +c Dy ... the publisher Engineering Mechanics - Statics Chapter MD = Mmax MD w1 = w1 = 100 w2 = 22 5 ab N m N m Assume that the maximum normal force in BC has been reached T = Pmax T2 d w2 = ( a + b) c ... from the publisher Engineering Mechanics - Statics Chapter b − Ay( b + c) + F1 ( a + b + c) + w b⎛ c + ⎞ + F2 c = ⎜ 2 ⎝ ⎠ F1 ( a + b + c) + w b⎛ c + ⎜ ⎝ Ay = b⎞ ⎟ + F2 c 2 b+c Ay = 4514 lb...
... Solution: L ⎛ θ ⎞ − 2L sin ⎛ θ ⎞ N = ⎟ ⎜ ⎟ A 22 cos ⎜ ΣMD = 0; 2W ΣΜC = 0; T L cos ⎜ ⎛ θ ⎞ − N L sin ⎛ θ ⎞ − W L cos ⎛ θ ⎞ = ⎟ ⎜ ⎟ ⎜ ⎟ A 222 W ⎛θ⎞ NA = cot ⎜ ⎟ 2 T=W Problem 6-113 ... from the publisher Engineering Mechanics - Statics F CG = F Chapter a F CG = 100 N b Sector gear : ⎞d = 2 ⎝ c +d ⎠ ΣMH = 0; F CG( d + e) − FAB⎛ ⎜ c ⎛ c2 + d2 ⎞ ⎟ F = 29 7. 62 N F AB = FCG ( d ... permission in writing from the publisher Engineering Mechanics - Statics F = Chapter W1 + W2 F = 1 02 lb Man: + ↑ Σ F y = 0; NC − W1 + ⎛F⎞ = ⎜ ⎟ ⎝ 2 NC = W1 − F NC = 72. 5 lb Problem 6-115 The piston C...
... ⎟ ⎝ 2 uAD = ⎛ −a ⎟ ⎜ ⎞ ⎜ ⎟ 2 ⎟ ⎛ a⎞ ⎜ ⎟ h +⎜ ⎟ ⎝ 2 ⎝ h ⎠ uBD = ⎛a⎟ ⎜ ⎞ 22 ⎟ a⎞ h +⎛ ⎟ ⎜h⎟ ⎜ ⎝ 2 ⎝ ⎠ uAC = ⎛−a ⎟ ⎜ ⎞ ⎜ 22 b ⎟ a⎞ 2 h +b +⎛ ⎟ ⎜ h ⎟ ⎜ ⎝ 2 ⎝ ⎠ uBC = ⎛a⎟ ⎜ ⎞ 22 b ... publisher Engineering Mechanics - Statics b −F CD − −b + a +b 22 b +c −c F AD − c −F − F DE − + FBD a +b +c a +b +c Chapter =0 b 2 b +c F DF F DF = F AD Joint B a −F BC − 2 a +b FBD = b 2 a +b ... publisher Engineering Mechanics - Statics Chapter Given Ay − w1 a − MA − w1 a a − d b +d F CD = d d +b Ax − b b +d b F CD2 a = 2 b +d d FCD = FCD − Bx = c c B y c − w2 =0 c FCD − w2 + B y = 2 b +d...
... the publisher Engineering Mechanics - Statics Chapter Given: F = 30 kN F = 20 kN F = 20 kN F = 40 kN a = 4m b = 4m Solution: −F a − F 3( 2a) − F 4( 3a) + Gy( 4a) = Gy = F2 + 2F + 3F4 Gy = 45 ... publisher = Chapter EngineeringMechanics - Statics Solution: Guess E y = lb F GJ = lb Given −F 2( a) − F3( 2a) − F4( 3a) + Ey( 4a) = −F 4( a) + Ey( 2a) + F GJ sin ( θ ) ( 2a) = ⎞ ⎛ Ey ⎟ ⎜ = Find ... Ax = (F1 − Ay)( 4a) + F2( 3a) + F3( 2a) + F4( a) = (F1 − Ay)( a) + Ax( c) − FBC ( c) = (F1 − Ay)( 2a) + F2( a) + ( A y − F 1) ( d) − F 2( a + d ) + a a +b F HG( c) + c 2 a +c b a +b FHC ( a +...
... the publisher Engineering Mechanics - Statics Chapter a = ft b = ft x1 = 1.5 ft x2 = 7.5 ft Solution: The maximum occurs when x = x2 ΣMA = 0; −F x2 + B x a = Bx = F x2 a B x = 1.4 62 × 10 lb + → ... the publisher Engineering Mechanics - Statics Chapter d = e = f = 12 g = Solution: Initial Guesses: NA = 20 lb NB = 10 lb MA = 30 lb ft Given f g ⎞ ⎞ ⎛ ⎛ ⎜ 2 ⎟ ( a + b) − NB ⎜ 2 ⎟ c = ⎝ f +g ... publisher Engineering Mechanics - Statics Chapter Given: W1 = 800 lb W2 = 450 lb W3 = 400 lb a = 2ft b = ft c = ft Solution: + → Σ Fx = 0; + ↑Σ Fy = 0; Dx = Dy − ( W1 + W2 + W3 ) = Dy = W1 + W2 + W3...
... 800 lb w2 = 500 lb ft ft a = 12 ft b = ft Solution: FR = a w1 + (w1 − w2)b + w2 b F R = 10.65 kip a 1 b b F R x = − a w1 + ( w1 − w2 ) b + w2 b 2 x = a b b − a w1 + ( w1 − w2 ) b + w2 b 3 2 FR x ... the publisher Engineering Mechanics - Statics ⎛α ⎞ ⎜ ⎟ ⎜ β ⎟ = acos ( −u) ⎜γ ⎟ ⎝ ⎠ Chapter ⎛ α ⎞ ⎛ 109 .22 6 ⎞ ⎜ ⎟ ⎜ ⎟ ⎜ β ⎟ = ⎜ 140 .20 6 ⎟ deg ⎜ γ ⎟ ⎝ 123 .28 6 ⎠ ⎝ ⎠ Problem 4-1 62 Determine the ... 800 N w2 = 20 0 N m m a = 2m b = 3m Solution: F R = w2 b + w1 a + x F R = w1 a w1 a x = a + (w1 − w2)b F R = 3.10 kN b b (w1 − w2)b⎛a + ⎞ + w2 b⎛a + ⎞ ⎜ ⎟ ⎜ ⎟ ⎝ ⎠ ⎝ a ⎛ b⎞ ⎛ b⎞ + ( w1 − w2 ) b⎜...