Chapter in. π(3.667)(1200) W = = = lbf W P 1.96(429.7)(6) FY 2(0.331) 2 V 282.7

Size: px
Start display at page:

Download "Chapter in. π(3.667)(1200) W = = = lbf W P 1.96(429.7)(6) FY 2(0.331) 2 V 282.7"

Transcription

1 Chaper d N = = = in Table 14-: Y = 0.1 Eq. (1-4): πdn π(.667)(100) V = = = 115 f/min 1 1 Eq. (14-4b): = = Eq. (1-5) : 15 = 000 = 000 = 49.7 lbf V 115 Eq. (14-7): 1.96(49.7)(6) = = = 76 psi = 7.6 kpsi FY (0.1) Ans. 14- d = N 18 = = 1.8 in 10 Table 14-: Y = 0.09 Eq. (1-4): π dn π (1.8)(600) V = = = 8.7 f/min 1 1 Eq. (14-4b): = = Eq. (1-5) : = 000 = 000 V 8.7 =.5 lbf Eq. (14-7): 1.6(.5)(10) = = = 940 psi = 9.4 kpsi FY 1.0(0.09) Ans. 14- d = mn = 1.5(18) =.5 mm Table 14-: Y = 0.09 V π dn π (.5)(10 )(1800) = = =.11 m/s Eq. (14-6b): = = Eq. (1-6): (0.5) 0.58 kn 5.8 N π dn π (.5)(1800) Eq. (14-8): 1.48(5.8) = = = 68.6 Ma FmY 1(1.5)(0.09) Ans. Shigley s MED, 10 h ediion Chaper 14 Soluions, age 1/9

2 14-4 d = mn = 8(16) = 18 mm Table 14-: Y = 0.96 V π dn π (18)(10 )(150) = = = m/s Eq. (14-6b): = = Eq. (1-6): (6) kn 5968 N π dn π (18)(150) Eq. (14-8): 1.165(5968) = = =.6 Ma FmY 90(8)(0.96) Ans d = mn = 1(16) = 16 mm Table 14-: Y = 0.96 V π dn π (16)(10 )(400) = = = 0.5 m/s Eq. (14-6b): = = Eq. (1-6): (0.15) kn N π dn π (16)(400) Eq. (14-8): F 1.055(447.6) = = = 10.6 mm my 150(1)(0.96) From Table 1-, use F = 11 mm or 1 mm, depending on availabiliy. Ans d = mn = (0) = 40 mm Table 14-: Y = 0. V π dn π (40)(10 )(00) = = = m/s Eq. (14-6b): = = Eq. (1-6): (0.5) kn 1194 N π dn π (40)(00) Eq. (14-8): F 1.069(1194) = = = my 75(.0)(0.) 6.4 mm From Table 1-, use F = 8 mm. Ans. Shigley s MED, 10 h ediion Chaper 14 Soluions, age /9

3 14-7 d = N 4 = = 4.8 in 5 Table 14-: Y = 0.7 Eq. (1-4): V π dn π (4.8)(50) = = = 6.8 f/min 1 1 Eq. (14-4b): = = Eq. (1-5) : 6 = 000 = 000 = 151 lbf V 6.8 Eq. (14-7): 1.05(151)(5) F = = =.46 in Y 0(10 )(0.7) Use F =.5 in Ans d = N 16 = = 4.0 in 4 Table 14-: Y = 0.96 Eq. (1-4): π dn π (4.0)(400) V = = = f/min 1 1 Eq. (14-4b): = = Eq. (1-5) : 0 = 000 = 000 = lbf V Eq. (14-7): 1.49(1575.6)(4) F = = =.9 in Y 1(10 )(0.96) Use F =.5 in Ans Try = 8 which gives d = 18/8 =.5 in and Y = Eq. (1-4): V π dn π (.5)(600) = = = f/min Eq. (14-4b): = = Eq. (1-5):.5 = 000 = 000 =.4 lbf V 5.4 Eq. (14-7): 1.95(.4)(8) F = = = 0.78 in Y 10(10 )(0.09) Using coarse ineger piches from Table 1-, he following able is formed. Shigley s MED, 10 h ediion Chaper 14 Soluions, age /9

4 d V F Oher consideraions may dicae he selecion. ood candidaes are = 8 (F = 7/8 in) and =10 (F = 1.5 in). Ans Try m = mm which gives d = (18) = 6 mm and Y = π dn π (6)(10 )(900) V = = = m/s Eq. (14-6b): = = (1.5) Eq. (1-6): = kn 884 N π dn = π (6)(900) = = 1.78(884) Eq. (14-8): F = = 4.4 mm 75()(0.09) Using he preferred module sizes from Table 1-: m d V K v F Shigley s MED, 10 h ediion Chaper 14 Soluions, age 4/9

5 Oher design consideraions may dicae he size selecion. For he presen design, m = mm (F = 5 mm) is a good selecion. Ans Eq. (14-4b): Eq. (1-6): N 0 N 50 d = = =.5 in, d = = = 6.5 in 8 8 π (.5)(100) V = = f/min = = = 000 = 000 = 504. lbf V Table 14-8: C = 100 psi [Noe: Using Eq. (14-1) can resul in wide variaion in p C p due o wide variaion in cas iron properies.].5sin sin 0 Eq. (14-1): r1 = = in, r = = in Eq. (14-14): C C K 1 1 v = p + F cosφ r r (504.) 1 1 = cos = 9.5(10 ) psi = 9.5 kpsi Ans. 1/ 1/ 14-1 d V = = 1. in, d = = 4 in 1 1 π(1.)(700) = = 44. f/min 1 Eq. (14-4b): Eq. (1-6): Table 14-8: = = = 000 = 000 = 0.6 lbf V 44. C = 100 psi [Noe: Using Eq. (14-1) can resul in wide variaion p in C p due o wide variaion in cas iron properies.] 1.sin 0 4 sin 0 Eq. (14-1): r1 = = 0.8 in, r = = in Eq. (14-14): Shigley s MED, 10 h ediion Chaper 14 Soluions, age 5/9

6 C 1/ 1.04(0.6) (10 ) = + = F cos (0.6) 1 1 F = in 100(10 ) + = cos Use F = 0.75 in Ans d = 5(4) = 10 mm, d = 5(48) = 40 mm p (10)(10 )(50) V π = = 0.14 m/s Eq. (14-6a): = = (10 ) =.18 π dn = π (10)(50) = where is in k and is in kn Table 14-8: C = 16 Ma [Noe: Using Eq. (14-1) can resul in wide variaion in p C p due o wide variaion in cas iron properies]. 10sin 0 40sin 0 Eq. (14-1): r1 = = 0.5 mm, r = = mm Eq. (14-14): ( ) 1.10(.18) = 16 + o 60 cos =.94 k Ans. 1/ Eq. (14-6a): d = 4(0) = 80 mm, d = 4() = 18 mm π (80)(10 )(1000) V = = m/s = =.7.05 = 60(10)(10 ).87 kn 87 N π (80)(1000) = = Table 14-8: C = 16 Ma [Noe: Using Eq. (14-1) can resul in wide variaion in p C p due o wide variaion in cas iron properies.] Shigley s MED, 10 h ediion Chaper 14 Soluions, age 6/9

7 80sin 0 18sin 0 Eq. (14-1): r1 = = 1.68 mm, r = = 1.89 mm.7(87) 1 1 Eq. (14-14): C = 16 + = 617 Ma Ans. 50 cos The pinion conrols he design. Bending Y = 0.0, Y = d = = in, d = =.500 in 1 1 πdn π(1.417)(55) V = = = f/min Eq. (14-4b): = = Eq. (6-8), p. 90: S e = 0.5(76) = 8.0 kpsi Eq. (6-19), p. 95: k a =.70(76) 0.65 = l = = = in d 1 Y (0.0) Eq. (14-): x = = = in (1) Eq. (b), p. 79: = 4lx = 4(0.1875)(0.079) = in Eq. (6-5), p. 97: d = hb = (0.1686) = 0.10 in e Eq. (6-0), p. 96: k b = = k c = k d = k e = 1 Accoun for one-way bending wih k f = (See Ex. 14-.) 1/ Eq. (6-18), p. 95: S e = 0.857(0.996)(1)(1)(1)(1.66)(8.0) = 5.84 kpsi For sress concenraion, find he radius of he roo fille (See Ex. 14-) r = f 0.05 in = 1 = From Fig. A-15-6, r r 0.05 = f = = d Approximae D/d = wih D/d = ; from Fig. A-15-6, K = From Fig. 6-0, wih S u = 76 kpsi and r = 0.05 in, q = 0.6. Shigley s MED, 10 h ediion Chaper 14 Soluions, age 7/9

8 Eq. (6-): K f = (1.68 1) = 1.4 Se 5.84 all = = = psi K n 1.4(.5) f d FY all 0.875(0.0)(16 850) = = = 0.4 lbf d 1.16(1) V 0.4(194.8) = = = 1.89 hp Ans ear ν 1 = ν = 0.9, E 1 = E = 0(10 6 ) psi Eq. (14-1): C p 1/ 1 = = π 6 0( 10 ) 85 psi d Eq. (14-1): r1 = sin φ = sin 0 = 0.4 in d.500 r = sinφ = sin 0 = 0.48 in = + = in r r Eq. (6-68), p. 7: ( S ) 8 = kpsi = [0.4(149) 10](10 ) = psi C 10 From he discussion and equaion developed on he boom of p. 7, ( SC ) C,all = = = 067 psi n cos 0 Eq. (14-14): = =.6 lbf (6.469) V.6(194.8) = = = 0.1 hp Ans Raing power (pinion conrols): 1 = 1.89 hp = 0.1 hp all = (min 1.89, 0.1) = 0.1 hp Ans. B Shigley s MED, 10 h ediion Chaper 14 Soluions, age 8/9

9 14-16 See rob soluion for equaion numbers. inion conrols: Y = 0., Y = Bending d = 0/ = in, d = 100/ =. in V = π dn / 1 = π (6.667)(870) / 1 = 1519 f/min = ( ) / 100 =.66 S e = 0.5(11) = 56.5 kpsi 0.65 ka =.70(11) = l =.5 / d =.5 / = 0.75 in x = (0.) / [()] = in = 4(0.75)(0.161) = in d e = (0.695) = in kb = (1.065 / 0.0) = 0.87 kc = kd = ke = 1 k f = 1.66 (See Ex. 14-.) S = 0.771(0.87)(1)(1)(1)(1.66)(56.5) = 6.1 kpsi e rf = 0.00 / = in r rf = = = d K = 1.75, q = 0.85, K f = 1.64 Se 6.1 all = = = 5.7 kpsi K n 1.64(1.5) f d FY all.5(0.)(5 700) = = = 04 lbf d.66() = V / 000 = 04(1519) / 000 = 140 hp Ans. ear Eq. (14-1): C p 1/ 1 = = π 6 0( 10 ) 85 psi Eq. (14-1): r 1 = (6.667/) sin 0 = in r = (./) sin 0 = in Eq. (6-68), p. 7: S C = [0.4(6) 10](10 ) = psi C,all = SC / nd = / 1.5 = psi Shigley s MED, 10 h ediion Chaper 14 Soluions, age 9/9

10 C,all F cosφ 1 = C p 1 / r1 + 1 / r cos 0 1 = / / = 110 lbf V 110(1519) = = = 5.0 hp Ans For 10 8 cycles (revoluions of he pinion), he power based on wear is 5.0 hp. Raing power (pinion conrols): 1 = 140 hp = 5.0 hp raed = min(140, 5.0) = 5.0 hp Ans See rob soluion for equaion numbers. iven: φ = 0, n = 1145 rev/min, m = 6 mm, F = 75 mm, N = 16 milled eeh, N = 0T, S u = 900 Ma, B = 60, n d =, Y = 0.96, and Y = inion bending d = mn = 6(16) = 96 mm d = 6(0) = 180 mm π dn π (96)(10 )(1145) V = = = 5.76 m/s 60 (60) = = S e = 0.5(900) = 450 Ma 0.65 ka = 4.51(900) = l =.5m =.5(6) = 1.5 mm x = Ym / = (0.96)6 / =.664 mm = 4lx = 4(1.5)(.664) = 1.0 mm d e = (1.0) = 4. mm kb = = kc = kd = ke = 1 k f = 1.66 (See Ex. 14-) S = 0.744(0.884)(1)(1)(1)(1.66)(450) = 491. Ma r f e = 0.00m = 0.00(6) = 1.8 mm r/d = r f / = 1.8/1 = 0.15, K = 1.68, q = 0.86, K f = 1.58 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 10/9

11 Se 491. all = = = K n f d ( ) 9. Ma FYm all 75(0.96)(6)(9.) Eq. (14-8): = = = N K Eq. (1-6): ear: inion and gear v π dn 16.9 π (96)(1145) = = = 94. k Ans Eq. (14-1): r 1 = (96/) sin 0 = 16.4 mm r = (180/) sin 0 = 0.78 mm 1 Eq. (14-1): C p = = 190 Ma π 07( 10 ) Eq. (6-68), p. 7: S C = 6.89[0.4(60) 10] = Ma C,all = SC / nd = = 568 Ma 1. Eq. (14-14): Eq. (1-6): 1/ F cosφ 1 C,all = C p K 1 / r1 + 1 / r v o cos 0 1 = = / / 0.78 π dn.469 π (96)(1145) = = = 0.0 k N Thus, wear conrols he gearse power raing; = 0.0 k. Ans N = 17 eeh, N = 51 eeh N 17 d = = =.8 in 6 51 d = = in 6 V = π d n / 1 = π (.8)(110) / 1 = 80.7 f/min Eq. (14-4b): = ( )/100 = 1.69 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 11/9

12 Sy all = = = n d psi Table 14-: Y = 0.0, Y = all (0.0)(45 000) Eq. (14-7): FY = = = 686 lbf K 1.69(6) Eq. (1-5): v V 686(80.7) = = = 67.6 hp Based on yielding in bending, he power is 67.6 hp. (a) inion faigue Bending Eq. (-1), p. 5: S u = 0.5 B = 0.5() = 116 kpsi Eq. (6-8), p. 90: S = 0.5S = 0.5(116) = 58 kpsi Eq. (6-19), p. 95: e k a u (116) = = Table 1-1, p. 688: l = + = = = 6 d d d 0.75 in Eq. (14-): x Y (0.0) = = = in (6) Eq. (b), p. 79: = 4lx = 4(0.75)(0.0758) = 0.7 in Eq. (6-5), p. 97: d = F = (0.7) = 0.66 in e Eq. (6-0), p. 96: k b = = k c = k d = k e = 1 Accoun for one-way bending wih k f = (See Ex. 14-.) Eq. (6-18): S e = 0.766(0.919)(1)(1)(1)(1.66)(58) = 67.8 kpsi For sress concenraion, find he radius of he roo fille (See Ex. 14-) r = f in = 6 = r r 0.05 Fig. A-15-6: = f = = d 0.8 Esimae D/d = by seing D/d =, K = Shigley s MED, 10 h ediion Chaper 14 Soluions, age 1/9

13 Fig. 6-0, p. 0: q = 0.86 Eq. (6-), p. 0: K f = 1 + (0.86)(1.68 1) = 1.58 Se 67.8 all = = = 1.5 kpsi K n 1.58() (b) inion faigue f d FY all (0.0)(1 500) = = = 18 lbf K 1.69(6) v d V 18(80.7) = = =. hp Ans ear Eq. (14-1): C p 1/ 1 = 6 = π[(1-0.9 ) / 0(10 )] 85 psi Eq. (14-1): d.8 o sin φ sin in r1 = = = d o r = sinφ = sin 0 = in = + =.750 in r1 r Eq. (6-68): ( S ) 8 = kpsi C 10 In erms of gear noaion B C = [0.4() 10]10 = psi e will inroduce he design facor of n d = and because i is a conac sress apply i o he load by dividing by n d =. (See p. 7.) c C,all = = = psi Solve Eq. (14-14) for : o cos 0 = 65 lbf (.750) = V 65(80.7) all = = = 6.67 hp Ans For 10 8 cycles (urns of pinion), he allowable power is 6.67 hp. Shigley s MED, 10 h ediion Chaper 14 Soluions, age 1/9

14 (c) ear faigue due o bending and wear Bending Eq. (14-): Y (0.410) x = = = in (6) Eq. (b), p. 79: = 4lx = 4(0.75)(0.106) = 0.9 in ± Eq. (6-5): d = F = (0.9) = in e Eq. (6-0): k b = = k c = k d = k e = 1 k f = (See Ex. 14-.) Eq. (6-18): S e = 0.766(0.911)(1)(1)(1)(1.66)(58) = 67. kpsi r d r f = = = Approximae D/d = by seing D/d = for Fig. A-15-6; K = Fig. 6-0: q = 0.8 Eq. (6-): K f = 1 + (0.8)(1.80 1) = 1.66 Se 67. all = = = 0. kpsi K n 1.66() f d FY all (0.410)(0 00) = = = 16 lbf K 1.69(6) v d V 16(80.7) all = = = 41.1 hp Ans The gear is hus sronger han he pinion in bending. ear Since he maerial of he pinion and he gear are he same, and he conac sresses are he same, he allowable power ransmission of boh is he same. Thus, all = 6.67 hp for 10 8 revoluions of each. As ye, we have no way o esablish S C for 10 8 / revoluions. (d) inion bending: 1 =. hp inion wear: = 6.67 hp ear bending: = 41.1 hp ear wear: 4 = 6.67 hp ower raing of he gear se is hus raed = min(., 6.67, 41.1, 6.67) = 6.67 hp Ans. Shigley s MED, 10 h ediion Chaper 14 Soluions, age 14/9

15 14-19 d = 16/6 =.667 in, d = 48/6 = 8 in π (.667)(00) V = = 09.4 f/min 1 000(5) = = lbf 09.4 Assuming uniform loading, K o = 1. / Eq. (14-8): Qv = 6, B = 0.5(1 6) = A = ( ) = Eq. (14-7): = = Table 14-: Y = 0.96, Y = From Eq. (a), Sec wih F = in ( Ks) = 1.19 = ( Ks) = 1.19 = From Eq. (14-0) wih C mc = 1 C p f = () = (.667) C = 1, C = 0.09 (Fig ), C = 1 K p m ma e m = 1 + 1[0.065(1) (1)] = Assuming consan hickness of he gears K B = 1 m = N /N = 48/16 = ih N (pinion) = 10 8 cycles and N (gear) = 10 8 /, Fig provides he relaions: ( YN ) = 1.558(10 ) = ( Y ) = 1.558(10 / ) = N Fig. 14-6: J = 0.7, J 0.8 Table 14-10: K R = 0.85 K T = C f = 1 Eq. (14-): Table 14-8: o o cos 0 sin 0 I = = (1) + 1 C p = 00 psi Shigley s MED, 10 h ediion Chaper 14 Soluions, age 15/9

16 Srengh: rade 1 seel wih B = B = 00 Fig. 14-: Fig. 14-5: (S ) = (S ) = 77.(00) = 8 60 psi (S c ) = (S c ) = (00) = psi Fig : (Z N ) = (10 8 ) 0.0 = (Z N ) = (10 8 /) 0.0 = 0.97 Sec. 14-1: B / B = 1 C = 1 inion ooh bending d K mk B Eq. (14-15): ) = Ko K s F J 6 (1.156)(1) = 787.8(1)(1.196)(1.088) 0.7 = psi Ans. Eq. (14-41): SYN / ( KT KR) ( SF ) = 8 60(0.977) / [(1)(0.85)] = = Ans. ear ooh bending 6 (1.156)(1) Eq. (14-15): ) = 787.8(1)(1.196)(1.097) = 94 psi Ans (0.996) / [(1)(0.85)] Eq. (14-41): ( SF ) = =.51 Ans. 94 inion ooh wear Eq. (14-16): ) K C C K K K d F I m f c = p o v s 1/ = (1)(1.196)(1.088).667() = psi Ans. 1/ Eq. (14-4): ScZ N /( KTK ) R 9 500(0.948) /[(1)(0.85)] ( S ) = = = 1.06 Ans. c Shigley s MED, 10 h ediion Chaper 14 Soluions, age 16/9

17 ear ooh wear 1/ 1/ ( K ) s c) = c) = (98 760) = psi Ans. ( Ks) (0.97)(1) /[(1)(0.85)] ( S ) = = 1.08 Ans The hardness of he pinion and he gear should be increased d =.5(0) = 50 mm, d =.5(6) = 90 mm πdn π(50)(10 )(100) V = = = m/s (10) = = N π(50)(10 )(100) ih no specific informaion given o indicae oherwise, assume K B = K o = Y θ = Z R = 1 Eq. (14-8): Qv = 6, B = 0.5(1 6) / = A = ( ) = (0.618) Eq. (14-7): = = Table 14-: Y = 0., Y = Similar o Eq. (a) of Sec bu for SI unis: C ma K s 1 = = 0.84 k b ( mf Y ) ( Ks) = (18) 0. = 1.00 use ( Ks) = (18) =1.007 use 1 Cmc = Ce = Cpm = 1 18 F = 18 / 5.4 = in, Cpf = 0.05 = (50) = + = (0.709) 0.765(10 )(0.709 ) 0.59 K = 1 + 1[0.011(1) (1)] = 1.7 Fig : (Y N ) = 1.558(10 8 ) = (Y N ) = 1.558(10 8 /1.8) = Fig. 14-6: (Y J ) = 0., (Y J ) = 0.8 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 17/9

18 Eq. (14-8): Y Z = ln(1 0.95) = o o cos 0 sin Eq. (14-): Z I = = 0.10 (1) Table 14-8: Z E = 191 Ma Srengh rade 1 seel, B = B = 00 Fig. 14-: (S ) = (S ) = 0.5(00) = Ma Fig. 14-5: (S c ) = (S c ) =.(00) + 00 = 644 Ma Fig : (Z N ) = (10 8 ) 0.0 = ( ) = (10 / 1.8) = Z N Fig. 14-1: / = 1 Z = C = 1 B B inion ooh bending 1 K K B Eq. (14-15): ) = KoKs bm Y Eq. (14-41) for SI: J 1 1.7(1) = 458.4(1)(1.099)(1) = 4.08 Ma Ans. 18(.5) 0. S Y N ( SF ) = = = 4.99 Ans. Y θ YZ (0.885) ear ooh bending 1 1.7(1) ) = 458.4(1)(1.099)(1) 7.4 Ma. 18(.5) 0.8 = Ans ( SF ) = 5.81 Ans. 7.4 = 1(0.885) inion ooh wear Eq. (14-16): ) Eq. (14-4) for SI: ear ooh wear K Z = Z K K K d b Z R c E o v s w1 I = (1)(1.099)(1) = Ma Ans. 50(18) 0.10 Sc Z NZ (1) ( S ) = = = 1.7 Ans. Y θ Y (0.885) c Z 1/ 1/ ( K ) s 1 c) = c) = (501.8) = Ma Ans. ( Ks) 1 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 18/9

19 (1) ( S ) = = 1.9 Ans (0.885) 14-1 = n cosψ = 6 cos 0 = eeh/in d = =.079 in, d = (.079) = 9.8 in π (.079)(00) V = = 41.8 f/min (5) = = 68. lbf, = = From rob : Y = 0.96, Y = ( Ks) = 1.088, ( Ks) = 1.097, KB = 1 m =, ( YN ) = 0.977, ( YN ) = 0.996, KR = 0.85 ( S ) = ( S ) = 8 60 psi, C = 1, ( S ) = ( S ) = psi c c ( Z ) = 0.948, ( Z ) = 0.97, C = 00 psi N N The pressure angle is: 1 an 0 φ = an =.80 cos0.079 ( rb ) = cos.8 = in, ( rb ) = ( rb ) = 4.58 in a = 1 / n = 1 / 6 = in Eq. (14-5): p 1/ 1/ Z = sin.8 = = Condiions O. K. for use p π = p cosφ = cos 0 = in 6 N n n Eq. (14-1): m N pn 0.49 = = = Z 0.95(0.7466) Shigley s MED, 10 h ediion Chaper 14 Soluions, age 19/9

20 Eq. (14-): I sin.8 cos.8 = (0.697) = Fig. 14-7: J 0.45, J 0.54 Fig. 14-8: Correcions are 0.94 and J = 0.45(0.94) = 0.4, J = 0.54(0.98) = 0.59 Cmc = 1, C pf = () = (.079) C = 1, C = 0.09, C = 1 K pm ma e m = 1 + (1)[0.055(1) (1)] = inion ooh bending (1) ) = 68.(1)(1.1)(1.088) = 6 psi Ans (0.977) / [1(0.85)] ( SF ) = = 5.14 Ans. 6 ear ooh bending (1) ) = 68.(1)(1.1)(1.097) = 5097 psi Ans (0.996) / [1(0.85)] ( SF ) = = 6.50 Ans inion ooh wear c) = (1)(1.1)(1.088) psi..078() = Ans (0.948) / [(1)(0.85)] ( S ) = = 1.54 Ans ear ooh wear 1/ 1/ c) = (67 700) = psi Ans (0.97) /[(1)(0.85)] ( S ) = = 1.57 Ans iven: R = 0.99 a 10 8 cycles, B = hrough-hardening rade 1, core and case, boh gears. N = 17T, N = 51T, Table 14-: Y = 0.0, Y = Shigley s MED, 10 h ediion Chaper 14 Soluions, age 0/9

21 Fig. 14-6: J = 0.9, J = 0.96 d = N / = 17 / 6 =.8 in, d = 51 / 6 = in. inion bending From Fig. 14-: ( S ) = B = 77.() = 0 74 psi Fig : Y N = 1.681(10 8 ) 0.0 = 0.98 Eq. (14-15): V = π d n / 1 = π (.8)(110 / 1) = 80.7 f/min KT = KR = 1, SF =, S = 0 74(0.98) all = = psi (1)(1) Qv = = = A = ( ) = K v / 5, B 0.5(1 5) = = K s = 1.19 = use 1 6 K = C = 1 + C ( C C + C C ) C C C C m m f mc p f p m ma e mc pf pm ma C = 1 e = 1 F = F 10d = () = (.8) = 1 = + = () 0.09(10 )( ) Km = 1 + 1[0.0581(1) (1)] = 1.17 KB = 1 FJ all = KoKsd KmKB (0.9)(14 61) = = 775 lbf 1(1.47)(1)(6)(1.17)(1) V 775(80.7) = = = 19.5 hp inion wear Shigley s MED, 10 h ediion Chaper 14 Soluions, age 1/9

22 Fig : Z N =.466N =.466(10 8 ) = m = 51 / 17 = Eq. (14-): o o cos 0 sin 0 I = = 1.05, C = Fig. 14-5: ( S ) 7 = Eq. (14-16): 0.99 c 10 B = () = psi (0.879) c,all = = psi (1)(1) FdI C K K K C c,all = p o s m f (.8)(0.105) = 00 1(1.47)(1)(1.167)(1) = 00 lbf V 00(80.7) = = = 7.55 hp The pinion conrols, herefore raed = 7.55 hp Ans. 14- l =.5/ d, x = Y / d.5 Y.674 = 4lx = 4 = Y d d d.674 de = F = F Y = d k b F Y / d F Y = = d F Y 1 F Y Ks = = 1.19 Ans. k b d 14-4 Y = 0.1, Y = 0.4, J = 0.45, J = 0.410, K o = 1.5. The service condiions are adequaely described by K o. Se S F = S = 1. d = / 4 = in d = 60 / 4 = in d Shigley s MED, 10 h ediion Chaper 14 Soluions, age /9

23 π (5.5)(1145) V = = 1649 f/min 1 inion bending ( S ) = = 77.(50) = 15 psi Eq. (14-17): ( ) B YN = 1.681[(10 )] = (0.8) all = = 678 psi 1(1)(1) / 0.5(1 6) B = = A = ( ) = K K C v s mc C ma = = = 1, C = 1 m F = F 10d.5 = (.5) = (5.5) = + = (.5) 0.09(10 )(.5 ) C e = 1 K = C = 1 + (1)[0.06(1) (1)] = 1.40 K m B m f = 1, K = 1 T 6 78(.5)(0.45) Eq. (14-15): 1 = = 1.5(1.54)(1)(4)(1.40) 151(1649) 1 = = hp lbf ear bending By similar reasoning, = 861 lbf and = 19.9 hp inion wear m = 60 / =.77 o o cos 0 sin 0.77 I = = ( S ) = (50) = psi 0.99 c ( Z N ) =.466[(10 )] = ( Z N ) =.466[(10 ) /.77] = (0.77) c,all) = = psi 1(1)(1) Shigley s MED, 10 h ediion Chaper 14 Soluions, age /9

24 c,all = FdI C K K K C p o s m f (5.5)(0.1176) = = 1061 lbf (1.54)(1)(1.4)(1) 1061(1649) = = 5.0 hp 000 ear wear Similarly, 4 = 118 lbf, 4 = 59.0 hp Raing raed = min( 1,,, 4) = min(157.5, 19.9, 5, 59) = 5 hp Ans. Noe differing capaciies. Can hese be equalized? 14-5 From rob. 14-4: = 151 lbf, = 861 lbf, = 1061 lbf, = 118 lbf 000Ko 000(1.5)(40) = = = 1000 lbf V inion bending: The facor of safey, based on load and sress, is ( S F) = = =.15 Ans ear bending based on load and sress 861 ( S F) = = =.86 Ans inion wear 1061 based on load: n = = = based on sress: ( S ) = 1.06 = 1.0 Ans. ear wear based on load: n 4 = = = Shigley s MED, 10 h ediion Chaper 14 Soluions, age 4/9

25 based on sress: ( S ) = 1.18 = 1.09 Ans. Facors of safey are used o assess he relaive hrea of loss of funcion.15,.86, 1.06, 1.18 where he hrea is from pinion wear. By comparison, he AMA safey facors (S F ), (S F ), (S ), (S ) are.15,.86, 1.0, 1.09 or.15,.86, /, / and he hrea is again from pinion wear. Depending on he magniude of he numbers, using S F and S as defined by AMA, does no necessarily lead o he same conclusion concerning hrea. Therefore be cauious Soluion summary from rob. 14-4: n = 1145 rev/min, K o = 1.5, rade 1 maerials, N = T, N = 60T, m =.77, Y = 0.1,Y = 0.4, J = 0.45, J = 0.410, d = 4T /in, F =.5 in, Qv = 6, (N c ) = (10 9 ), R = 0.99, K m = 1.40, K T = 1, K B = 1, d = in, d = in, V = 1649 f/min, = 1.54, (K s ) = (K s ) = 1, (Y N ) = 0.8, (Y N ) = 0.859, K R = 1 inion B : 50 core, 90 case ear B : 50 core, 90 case Bending = 6 78 psi ( S ) all) = 15 psi all) = psi ( ) S = 15 psi = 151 lbf, = hp = 861 lbf, = 19.9 hp 1 1 ear φ = I = Z N = o 0, , ( ) 0.77 ( Z ) = 0.769, C = 00 psi N ( S ) = S = (90) = psi c c (0.77) c,all) = = psi 1(1)(1) (0.769) c,all) = = psi 1(1)(1) (1649) = (1061) = 11 lbf, = = hp (1649) = (118) = 54 lbf, = = hp (0.769) Shigley s MED, 10 h ediion Chaper 14 Soluions, age 5/9

26 Raed power raed = min(157.5, 19.9, 105.6, 117.6) = hp Ans. rob. 14-4: raed = min(157.5, 19.9, 5.0, 59.0) = 5 hp The raed power approximaely doubled The gear and he pinion are 910 grade 1, carburized and case-hardened o obain Brinell 85 core and Brinell case. Table 14-: ( S ) 7 = psi Modificaion of S by (Y N ) = 0.8 produces ) = psi, all Similarly for (Y N ) = ) = psi, and all = 4569 lbf, = 8 hp = 5668 lbf, = 8 hp 1 1 From Table 14-8, C = 00 psi. Also, from Table 14-6: p ( S ) = psi 0.99 c 10 7 Modificaion of S c by Y N produces and c,all) = psi ) = psi c,all = 489 lbf, = 14. hp = 767 lbf, = 18. hp 4 4 Raing raed = min(8, 8, 14, 18) = 14 hp Ans. Shigley s MED, 10 h ediion Chaper 14 Soluions, age 6/9

27 14-8 rade, 910 carburized and case-hardened o 85 core and 580 case in rob Summary: Table 14-: ( S ) 7 = psi and i follows ha all) = psi ) = psi all = 5400 lbf, = 70 hp = 6699 lbf, = 5 hp 1 1 From Table 14-8, C = 00 psi. Also, from Table 14-6: p Consequenly, S c = psi ) = psi c,all ) = psi c,all = 4801 lbf, = 40 hp = 57 lbf, = 67 hp 4 4 Raing raed = min(70, 5, 40, 67) = 40 hp. Ans iven: n = 1145 rev/min, K o = 1.5, N = T, N = 60T, m =.77, d =.75 in, d = 7.5 in, Y = 0.1,Y = 0.4, J = 0.5, J = 0.405, = 8T /in, F = 1.65 in, B = 50, case and core, boh gears. C m = 1, F/d = , C f = , C pm = 1, C ma = 0.15, C e = 1, K m = 1.194, K T = 1, K B = 1, K s = 1,V = 84 f/min, (Y N ) = 0.818, (Y N ) = 0.859, K R = 1, I = ( S ) = 15 psi all) = psi ) = psi all and i follows ha = 879. lbf, = 1.97 hp = 1098 lbf, = 7.4 hp 1 1 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 7/9

28 For wear = 04 lbf, = 7.59 hp = 40 lbf, = 8.50 hp 4 4 Raing raed = min(1.97, 7.4, 7.59, 8.50) = 7.59 hp In rob. 14-4, raed = 5 hp. Thus, The ransmied load raing is In rob = 0.14 =, no Ans raed = min(879., 1098, 04, 40) = 04 lbf raed = 1061 lbf Thus = =, no Ans S = S = 1, d = 4, J = 0.45, J = 0.410, K o = 1.5 Bending Table 14-4: ( S ) 7 = psi (1) all) = all) = = psi 1(1)(1) allfj 1 000(.5)(0.45) 1 = = = 15 lbf Ko Ksd KmKB 1.5(1.54)(1)(4)(1.4)(1) 15(1649) 1 = = 76.6 hp 000 = 1 J / J = 15(0.410) / 0.45 = 18 lbf = J / J = 76.6(0.410) / 0.45 = 91.0 hp 1 ear Table 14-8: C p = 1960 psi Table 14-7: ( S ) 7 = psi = ) = ) 0.99 c 10 c,all c,all Shigley s MED, 10 h ediion Chaper 14 Soluions, age 8/9

29 c,all p = Cp KoKsKmC f 4 4 ) Fd I (5.5)(0.1176) = = 195 lbf (1.54)(1)(1.4)(1) = = 195 lbf = 195(1649) = = 64.7 hp 000 Raing raed = min(76.7, 94.4, 64.7, 64.7) = 64.7 hp Ans. Noice ha he balance beween bending and wear power is improved due o CI s more favorable S c /S raio. Also noe ha he life is 10 7 pinion revoluions which is (1/00) of (10 9 ). Longer life goals require power de-raing From Table A-4a, E av = 11.8(10 6 ) Mpsi For φ = 14.5 and B = 156 For φ = 0 S C 1.4(81) S = = psi C 6 sin14.5 / [11.8(10 )] 1.4(11) = = psi 6 sin 0 / [11.8(10 )] SC = 0.(156) = 49.9 kpsi The firs wo calculaions were approximaely 4 percen higher. 14- rograms will vary. 14- ( Y ) = 0.977, ( Y ) = N N ( S ) = ( S ) = 8.(50) = 75 psi 75(0.977) all) = = psi 1(0.85) 7 615(1.5)(0.4) 1 = = 1558 lbf 1(1.404)(1.04)(8.66)(1.08)(1) 1558(95) 1 = = 4.7 hp 000 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 9/9

30 75(0.996) all) = = 8 46 psi 1(0.85) 8 46(1.5)(0.546) = = 1(1.404)(1.04)(8.66)(1.08)(1) 007(95) = = 56. hp 000 ( Z ) = 0.948, ( Z ) = 0.97 N N 007 lbf Table 14-6: ( S ) 7 = psi 0.99 c (1) c,allow) = = psi 1(0.85) (1.5)(0.195) = = 074 lbf 00 1(1.404)(1.04) 074(95) = = 58.1 hp c,allow) = (167 94) = psi (1.5)(0.195) 4 = = 167 lbf 00 1(1.404)(1.05) 167(95) 4 = = 60.7 hp 000 raed = min(4.7, 56., 58.1, 60.7) = 4.7 hp Ans. inion bending is conrolling ( Y N ) = 1.681(10 ) = ( Y N ) = 1.681(10 /.059) = 0.96 Table 14-: S = psi (0.98) all) = = psi 1(0.85) (1.5)(0.4) 1 = = 1(1.404)(1.04)(8.66)(1.08)(1) 487(95) 1 = = 69.7 hp all) = (60 047) = 6 47 psi lbf Shigley s MED, 10 h ediion Chaper 14 Soluions, age 0/9

31 = (487) = 58 lbf = (69.7) = 91. hp 487 Table 14-6: S c = psi ( ) =.466(10 ) = Z N ( Z N ) =.466(10 /.059) = (0.8790) c,all) = = psi 1(0.85) (1.5)(0.195) = = 568 lbf 00 1(1.404)(1.04) 568(95) = = 7.0 hp c,all) = ( ) = psi = (568) = 886 lbf (95) 4 = = 80.9 hp 000 raed = min(69.7, 91., 7, 80.9) = 69.7 hp Ans. inion bending conrolling 14-5 (Y N ) = 0.98, (Y N ) = 0.96 (See rob. 14-4) Table 14-: S = psi (0.98) all) = = psi 1(0.85) (1.5)(0.4) 1 = = 99 lbf 1(1.404)(1.04)(8.66)(1.08) 99(95) 1 = = 8.4 hp (0.96) all) = = psi 1(0.85) = (99) = 850 lbf = (8.4) = 108 hp 99 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 1/9

32 Table 14-6: S c = psi ( Z ) = , ( Z ) = N N 5 000(0.879) c,all) = = 676 psi 1(0.85) (1.5)(0.195) = = 401 lbf 00 1(1.404)(1.04) 401(95) = = 11.5 hp c,all) = ( 676) = psi = (401) = 4509 lbf (95) 4 = = 16 hp 000 raed = min(8.4, 108, 11.5, 16) = 8.4 hp Ans. The bending of he pinion is he conrolling facor = eeh/in, d = 8 in, N = d = 8 () = 16 eeh π π F = 4 p = 4 = 4 = π o o M = 0 = 10(00) cos 0 4F cos0 x F B = 750 lbf o o = F B cos 0 = 750cos 0 = 705 lbf n = 400 / = 100 rev/min π dn π (8)(100) V = = = 51 f/min 1 1 e will obain all of he needed facors, roughly in he order presened in he exbook. B Fig. 14-: S = 10(00) = psi Fig. 14-5: S c = 49(00) = psi Fig. 14-6: J = 0.7 Eq. (14-): o o cos 0 sin 0 I = = (1) + 1 Table 14-8: C p = 00 psi Assume a ypical qualiy number of 6. / / Eq. (14-8): B = 0.5(1 Q ) = 0.5(1 6) = v Shigley s MED, 10 h ediion Chaper 14 Soluions, age /9

33 Eq. (14-7): A = (1 B) = ( ) = K v B A + V = = = 1.65 A To esimae a size facor, ge he Lewis Form Facor from Table 14-, Y = From Eq. (a), Sec , F Y π 0.96 Ks = 1.19 = 1.19 = 1. The load disribuion facor is applicable for sraddle-mouned gears, which is no he case here since he gear is mouned ouboard of he bearings. Lacking anyhing beer, we will use he load disribuion facor as a rough esimae. Eq. (14-1): C mc = 1 (uncrowned eeh) Eq. (14-): π C p f = ( π ) = (8) Eq. (14-): C pm = 1.1 Fig : C ma = 0. (commercial enclosed gear uni) Eq. (14-5): C e = 1 Eq. (14-0): K m = 1 + 1[0.1196(1.1) + 0.(1)] = 1.6 For he sress-cycle facors, we need he desired number of load cycles. N = h (100 rev/min)(60 min/h) = 1.1 (10 9 ) rev Fig : Y N = 0.9 Fig : Z N = 0.8 K = ln 1 R = ln = Eq. 14-8: ( ) ( ) R ih no specific informaion given o indicae oherwise, assume K o = K B = K T = C f = 1 Tooh bending d KmK B Eq. (14-15): = KoK s F J (1.6)(1) = 705(1)(1.65)(1.) = 94 psi π 0.7 Eq. (14-41): S F SYN / ( KT KR) = (0.9) / [(1)(0.885)] = = 0.8 Ans. 94 Shigley s MED, 10 h ediion Chaper 14 Soluions, age /9

34 Tooh wear Eq. (14-16): K C m f c = C p Ko Ks d F I (1)(1.65)(1.) = 8( π ) = psi Since gear B is a pinion, C is no used in Eq. (14-4) (see p. 75), where S = S Z / ( K K ) c N T R c (0.8) / [(1)(0.885)] = =.9 Ans m = mm/ooh, d = 00 mm N = d/m = 00 / = 16 eeh F = b = 4 p = 4 π m = 4π = 6 mm M x 1/ ( ) ( ) o = 0 = 00(11) cos 0 150F cos5 F B =.81 kn o o = F B cos 5 =.81cos 5 = 0.67 kn n = 1800 / = 900 rev/min π dn π (0.00)(900) V = = = m/s e will obain all of he needed facors, roughly in he order presened in he exbook. B o 1/ Fig. 14-: S = 0.70(00) + 11 = 4 Ma Fig. 14-5: S c =.41(00) + 7 = 960 Ma Fig. 14-6: J = Y J = 0.7 Eq. (14-): o o cos 0 sin 0 5 I = Z I = = (1) Table 14-8: Z E = 191 Ma 0.14 Assume a ypical qualiy number of 6. / / Eq. (14-8): B = 0.5(1 Qv ) = 0.5(1 6) = A = (1 B) = ( ) = Eq. (14-7): K v B A + 00V (14.14) = = = 1.69 A To esimae a size facor, ge he Lewis Form Facor from Table 14-, Y = Shigley s MED, 10 h ediion Chaper 14 Soluions, age 4/9

35 Similar o Eq. (a) of Sec bu for SI unis: K s 1 = = 0.84 k b ( mf Y ) Ks = (6) 0.96 = 1.8 Conver he diameer and facewidh o inches for use in he load-disribuion facor equaions. d = 00/5.4 = in, F = 6/5.4 = 9.9 in Eq. (14-1): C mc = 1 (uncrowned eeh) Eq. (14-): 9.9 C pf = (9.9) = (11.81) Eq. (14-): C pm = 1.1 Fig : C ma = 0.7 (commercial enclosed gear uni) Eq. (14-5): C e = 1 Eq. (14-0): K = K = 1 + 1[0.157(1.1) + 0.7(1)] = 1.44 m For he sress-cycle facors, we need he desired number of load cycles. N = h (900 rev/min)(60 min/h) = 6.48 (10 8 ) rev Fig : Y N = 0.9 Fig : Z N = 0.85 K = ln 1 R = ln = Eq. 14-8: ( ) ( ) R ih no specific informaion given o indicae oherwise, assume K o = K B = K T = Z R = 1. Tooh bending Eq. (14-15): 1 = KoKs bm B K K Y J 1 (1.44)(1) = 0 670(1)(1.69)(1.8) = 5.9 Ma 6(18.75) 0.7 Eq. (14-41): S F SYN / ( KT KR) = 4(0.9) / [(1)(0.955)] = = Ans. Tooh wear Eq. (14-16): K Z R c = ZE KoKs d w1 b Z I 1/ Shigley s MED, 10 h ediion Chaper 14 Soluions, age 5/9

36 = (1)(1.69)(1.8) 00(6) 0.14 = 498 Ma Since gear B is a pinion, C is no used in Eq. (14-4) (see p. 757), where ScZ N / ( KT KR) S = c 960(0.85) / [(1)(0.955)] = = 1.7 Ans From he soluion o rob. 1-40, n = 191 rev/min, = 1600 N, d = 15 mm, N = 15 eeh, m = 8. mm/ooh. F = b = 4 p = 4 π m = 4π 8. = 105 mm ( ) ( ) π dn π (0.15)(191) V = = = 1.5 m/s e will obain all of he needed facors, roughly in he order presened in he exbook. 1/ Table 14-: S = 65 kpsi = 448 Ma Table 14-6: S c = 5 kpsi = 1550 Ma Fig. 14-6: J = Y J = 0.5 Eq. (14-): o o cos 0 sin 0 I = Z I = = (1) + 1 Table 14-8: Z E = 191 Ma Assume a ypical qualiy number of Eq. (14-8): Eq. (14-7): / / B = 0.5(1 Qv ) = 0.5(1 6) = A = (1 B) = ( ) = K v B A + 00V (1.5) = = = 1.1 A To esimae a size facor, ge he Lewis Form Facor from Table 14-, Y = Similar o Eq. (a) of Sec bu for SI unis: K s 1 = = 0.84 k b ( mf Y ) Ks = (105) 0.90 = 1.17 Conver he diameer and facewidh o inches for use in he load-disribuion facor Shigley s MED, 10 h ediion Chaper 14 Soluions, age 6/9

37 equaions. d = 15/5.4 = 4.9 in, F = 105/5.4 = 4.1 in Eq. (14-1): C mc = 1 (uncrowned eeh) Eq. (14-): 4.1 C pf = (4.1) = (4.9) Eq. (14-): C pm = 1 Fig : C ma = 0. (open gearing) Eq. (14-5): C e = 1 Eq. (14-0): K = K = 1 + 1[0.0981(1) + 0.(1)] = 1.4 m For he sress-cycle facors, we need he desired number of load cycles. N = h (191 rev/min)(60 min/h) = 1.4 (10 8 ) rev Fig : Y N = 0.95 Fig : Z N = 0.88 K = ln 1 R = ln = Eq. 14-8: ( ) ( ) R ih no specific informaion given o indicae oherwise, assume K o = K B = K T = Z R = 1. Tooh bending Eq. (14-15): 1 = KoKs bm B K K Y 1 (1.4)(1) = 1600(1)(1.1)(1.17) = 14.7 Ma 105(8.) 0.5 Since gear is a pinion, C is no used in Eq. (14-4) (see p. 75), where J Tooh wear Eq. (14-16): S F SYN / ( KT KR) = 448(0.95) / [(1)(0.885)] = =.7 Ans K Z R c = ZE KoKs d w1 b Z I = (1)(1.1)(1.17) 15(105) = 89 Ma 1/ 1/ ScZN / ( KTKR) Eq. (14-4): S = c 1550(0.88) / [(1)(0.885)] = = 5. Ans 89 Shigley s MED, 10 h ediion Chaper 14 Soluions, age 7/9

38 14-9 From he soluion o rob. 1-41, n = (70) = 140 rev/min, = 180 lbf, d = 5 in N = 15 eeh, = eeh/in. π π F = 4 p = 4 = 4 = 4. in π dn π (5)(140) V = = = 18. f/min 1 1 e will obain all of he needed facors, roughly in he order presened in he exbook. Table 14-: S = 65 kpsi Table 14-6: S c = 5 kpsi Fig. 14-6: J = 0.5 Eq. (14-): o o cos 0 sin 0 I = = (1) + 1 Table 14-8: C p = 00 psi Assume a ypical qualiy number of Eq. (14-8): Eq. (14-7): / / B = 0.5(1 Qv ) = 0.5(1 6) = A = (1 B) = ( ) = K v B A + V = = = 1.18 A To esimae a size facor, ge he Lewis Form Facor from Table 14-, Y = From Eq. (a), Sec , F Y Ks = 1.19 = 1.19 = 1.17 Eq. (14-1): C mc = 1 (uncrowned eeh) Eq. (14-): 4. C pf = (4.) = (5) Eq. (14-): C pm = 1 Fig : C ma = 0. (Open gearing) Eq. (14-5): C e = 1 Eq. (14-0): K m = 1 + 1[0.099(1) + 0.(1)] = 1.4 For he sress-cycle facors, we need he desired number of load cycles. N = h (140 rev/min)(60 min/h) = 1. (10 8 ) rev Fig : Y N = 0.95 Fig : Z N = 0.88 K = ln 1 R = ln = Eq. 14-8: ( ) ( ) R ih no specific informaion given o indicae oherwise, assume K o = K B = K T = C f = 1. Shigley s MED, 10 h ediion Chaper 14 Soluions, age 8/9

39 Tooh bending d KmK B Eq. (14-15): = KoK s F J (1.4)(1) = 180(1)(1.18)(1.17) = 1010 psi Eq. (14-41): S F SYN / ( KT KR) = (0.95) / [(1)(0.955)] = = Ans. Tooh wear Eq. (14-16): K C m f c = C p Ko Ks d F I = (1)(1.18)(1.17) 5(4.) = psi 1/ 1/ Since gear B is a pinion, C is no used in Eq. (14-4) (see p. 75), where S ScZN / ( KTKR) = c 5 000(0.88) / [(1)(0.955)] = = 7.8 Ans Shigley s MED, 10 h ediion Chaper 14 Soluions, age 9/9

Chapter = For one gear straddle-mounted, the load-distribution factor is:

Chapter = For one gear straddle-mounted, the load-distribution factor is: Chaper 15 15-1 iven: Uncrowned, hrough-hardened 300 Brinell core and case, rade 1, N C 10 9 rev of pinion a R 0.999, N 0 eeh, N 60 eeh, Qv 6, d 6 eeh/in, normal pressure angle 0, shaf angle 90, n p 900

More information

Involute Gear Tooth Bending Stress Analysis

Involute Gear Tooth Bending Stress Analysis Involue Gear Tooh Bending Sress Analysis Lecure 21 Engineering 473 Machine Design Gear Ineracion Line of Ceners Line Tangen o s Line Normal o Line of Ceners 1 s Close Up of Meshed Teeh Line of Conac W

More information

At the end of this lesson, the students should be able to understand

At the end of this lesson, the students should be able to understand Insrucional Objecives A he end of his lesson, he sudens should be able o undersand Sress concenraion and he facors responsible. Deerminaion of sress concenraion facor; experimenal and heoreical mehods.

More information

20. Applications of the Genetic-Drift Model

20. Applications of the Genetic-Drift Model 0. Applicaions of he Geneic-Drif Model 1) Deermining he probabiliy of forming any paricular combinaion of genoypes in he nex generaion: Example: If he parenal allele frequencies are p 0 = 0.35 and q 0

More information

Chapter 2. First Order Scalar Equations

Chapter 2. First Order Scalar Equations Chaper. Firs Order Scalar Equaions We sar our sudy of differenial equaions in he same way he pioneers in his field did. We show paricular echniques o solve paricular ypes of firs order differenial equaions.

More information

236 CHAPTER 3 Torsion. Strain Energy in Torsion

236 CHAPTER 3 Torsion. Strain Energy in Torsion 36 CHAPER 3 orsion Srain Energy in orsion Problem 3.9-1 A solid circular bar of seel (G 11. 1 6 psi) wih lengh 3 in. and diameer d 1.75 in. is subjeced o pure orsion by orques acing a he ends (see figure).

More information

Final Spring 2007

Final Spring 2007 .615 Final Spring 7 Overview The purpose of he final exam is o calculae he MHD β limi in a high-bea oroidal okamak agains he dangerous n = 1 exernal ballooning-kink mode. Effecively, his corresponds o

More information

MA 214 Calculus IV (Spring 2016) Section 2. Homework Assignment 1 Solutions

MA 214 Calculus IV (Spring 2016) Section 2. Homework Assignment 1 Solutions MA 14 Calculus IV (Spring 016) Secion Homework Assignmen 1 Soluions 1 Boyce and DiPrima, p 40, Problem 10 (c) Soluion: In sandard form he given firs-order linear ODE is: An inegraing facor is given by

More information

Errata (1 st Edition)

Errata (1 st Edition) P Sandborn, os Analysis of Elecronic Sysems, s Ediion, orld Scienific, Singapore, 03 Erraa ( s Ediion) S K 05D Page 8 Equaion (7) should be, E 05D E Nu e S K he L appearing in he equaion in he book does

More information

MECHANICS OF MATERIALS Poisson s Ratio

MECHANICS OF MATERIALS Poisson s Ratio Poisson s Raio For a slender bar subjeced o axial loading: ε x x y 0 The elongaion in he x-direcion i is accompanied by a conracion in he oher direcions. Assuming ha he maerial is isoropic (no direcional

More information

Some Basic Information about M-S-D Systems

Some Basic Information about M-S-D Systems Some Basic Informaion abou M-S-D Sysems 1 Inroducion We wan o give some summary of he facs concerning unforced (homogeneous) and forced (non-homogeneous) models for linear oscillaors governed by second-order,

More information

ODEs II, Lecture 1: Homogeneous Linear Systems - I. Mike Raugh 1. March 8, 2004

ODEs II, Lecture 1: Homogeneous Linear Systems - I. Mike Raugh 1. March 8, 2004 ODEs II, Lecure : Homogeneous Linear Sysems - I Mike Raugh March 8, 4 Inroducion. In he firs lecure we discussed a sysem of linear ODEs for modeling he excreion of lead from he human body, saw how o ransform

More information

DESIGN OF TENSION MEMBERS

DESIGN OF TENSION MEMBERS CHAPTER Srcral Seel Design LRFD Mehod DESIGN OF TENSION MEMBERS Third Ediion A. J. Clark School of Engineering Deparmen of Civil and Environmenal Engineering Par II Srcral Seel Design and Analysis 4 FALL

More information

Module 2 F c i k c s la l w a s o s f dif di fusi s o i n

Module 2 F c i k c s la l w a s o s f dif di fusi s o i n Module Fick s laws of diffusion Fick s laws of diffusion and hin film soluion Adolf Fick (1855) proposed: d J α d d d J (mole/m s) flu (m /s) diffusion coefficien and (mole/m 3 ) concenraion of ions, aoms

More information

Introduction to AC Power, RMS RMS. ECE 2210 AC Power p1. Use RMS in power calculations. AC Power P =? DC Power P =. V I = R =. I 2 R. V p.

Introduction to AC Power, RMS RMS. ECE 2210 AC Power p1. Use RMS in power calculations. AC Power P =? DC Power P =. V I = R =. I 2 R. V p. ECE MS I DC Power P I = Inroducion o AC Power, MS I AC Power P =? A Solp //9, // // correced p4 '4 v( ) = p cos( ω ) v( ) p( ) Couldn' we define an "effecive" volage ha would allow us o use he same relaionships

More information

Combined Bending with Induced or Applied Torsion of FRP I-Section Beams

Combined Bending with Induced or Applied Torsion of FRP I-Section Beams Combined Bending wih Induced or Applied Torsion of FRP I-Secion Beams MOJTABA B. SIRJANI School of Science and Technology Norfolk Sae Universiy Norfolk, Virginia 34504 USA sirjani@nsu.edu STEA B. BONDI

More information

23.2. Representing Periodic Functions by Fourier Series. Introduction. Prerequisites. Learning Outcomes

23.2. Representing Periodic Functions by Fourier Series. Introduction. Prerequisites. Learning Outcomes Represening Periodic Funcions by Fourier Series 3. Inroducion In his Secion we show how a periodic funcion can be expressed as a series of sines and cosines. We begin by obaining some sandard inegrals

More information

6.003 Homework #8 Solutions

6.003 Homework #8 Solutions 6.003 Homework #8 Soluions Problems. Fourier Series Deermine he Fourier series coefficiens a k for x () shown below. x ()= x ( + 0) 0 a 0 = 0 a k = e /0 sin(/0) for k 0 a k = π x()e k d = 0 0 π e 0 k d

More information

Solutions from Chapter 9.1 and 9.2

Solutions from Chapter 9.1 and 9.2 Soluions from Chaper 9 and 92 Secion 9 Problem # This basically boils down o an exercise in he chain rule from calculus We are looking for soluions of he form: u( x) = f( k x c) where k x R 3 and k is

More information

Math 333 Problem Set #2 Solution 14 February 2003

Math 333 Problem Set #2 Solution 14 February 2003 Mah 333 Problem Se #2 Soluion 14 February 2003 A1. Solve he iniial value problem dy dx = x2 + e 3x ; 2y 4 y(0) = 1. Soluion: This is separable; we wrie 2y 4 dy = x 2 + e x dx and inegrae o ge The iniial

More information

14 Autoregressive Moving Average Models

14 Autoregressive Moving Average Models 14 Auoregressive Moving Average Models In his chaper an imporan parameric family of saionary ime series is inroduced, he family of he auoregressive moving average, or ARMA, processes. For a large class

More information

12/25/ :27 PM. Chapter 14. Spur and Helical Gears. Mohammad Suliman Abuhaiba, Ph.D., PE

12/25/ :27 PM. Chapter 14. Spur and Helical Gears. Mohammad Suliman Abuhaiba, Ph.D., PE Chapter 14 Spur and Helical Gears 1 2 The Lewis Bending Equation Equation to estimate bending stress in gear teeth in which tooth form entered into the formulation: 3 The Lewis Bending Equation Assume

More information

3.1.3 INTRODUCTION TO DYNAMIC OPTIMIZATION: DISCRETE TIME PROBLEMS. A. The Hamiltonian and First-Order Conditions in a Finite Time Horizon

3.1.3 INTRODUCTION TO DYNAMIC OPTIMIZATION: DISCRETE TIME PROBLEMS. A. The Hamiltonian and First-Order Conditions in a Finite Time Horizon 3..3 INRODUCION O DYNAMIC OPIMIZAION: DISCREE IME PROBLEMS A. he Hamilonian and Firs-Order Condiions in a Finie ime Horizon Define a new funcion, he Hamilonian funcion, H. H he change in he oal value of

More information

Math 10B: Mock Mid II. April 13, 2016

Math 10B: Mock Mid II. April 13, 2016 Name: Soluions Mah 10B: Mock Mid II April 13, 016 1. ( poins) Sae, wih jusificaion, wheher he following saemens are rue or false. (a) If a 3 3 marix A saisfies A 3 A = 0, hen i canno be inverible. True.

More information

6.2 Transforms of Derivatives and Integrals.

6.2 Transforms of Derivatives and Integrals. SEC. 6.2 Transforms of Derivaives and Inegrals. ODEs 2 3 33 39 23. Change of scale. If l( f ()) F(s) and c is any 33 45 APPLICATION OF s-shifting posiive consan, show ha l( f (c)) F(s>c)>c (Hin: In Probs.

More information

AP Chemistry--Chapter 12: Chemical Kinetics

AP Chemistry--Chapter 12: Chemical Kinetics AP Chemisry--Chaper 12: Chemical Kineics I. Reacion Raes A. The area of chemisry ha deals wih reacion raes, or how fas a reacion occurs, is called chemical kineics. B. The rae of reacion depends on he

More information

Chapter 3 Boundary Value Problem

Chapter 3 Boundary Value Problem Chaper 3 Boundary Value Problem A boundary value problem (BVP) is a problem, ypically an ODE or a PDE, which has values assigned on he physical boundary of he domain in which he problem is specified. Le

More information

CHAPTER 2 Signals And Spectra

CHAPTER 2 Signals And Spectra CHAPER Signals And Specra Properies of Signals and Noise In communicaion sysems he received waveform is usually caegorized ino he desired par conaining he informaion, and he undesired par. he desired par

More information

V L. DT s D T s t. Figure 1: Buck-boost converter: inductor current i(t) in the continuous conduction mode.

V L. DT s D T s t. Figure 1: Buck-boost converter: inductor current i(t) in the continuous conduction mode. ECE 445 Analysis and Design of Power Elecronic Circuis Problem Se 7 Soluions Problem PS7.1 Erickson, Problem 5.1 Soluion (a) Firs, recall he operaion of he buck-boos converer in he coninuous conducion

More information

23.5. Half-Range Series. Introduction. Prerequisites. Learning Outcomes

23.5. Half-Range Series. Introduction. Prerequisites. Learning Outcomes Half-Range Series 2.5 Inroducion In his Secion we address he following problem: Can we find a Fourier series expansion of a funcion defined over a finie inerval? Of course we recognise ha such a funcion

More information

t is a basis for the solution space to this system, then the matrix having these solutions as columns, t x 1 t, x 2 t,... x n t x 2 t...

t is a basis for the solution space to this system, then the matrix having these solutions as columns, t x 1 t, x 2 t,... x n t x 2 t... Mah 228- Fri Mar 24 5.6 Marix exponenials and linear sysems: The analogy beween firs order sysems of linear differenial equaions (Chaper 5) and scalar linear differenial equaions (Chaper ) is much sronger

More information

System of Linear Differential Equations

System of Linear Differential Equations Sysem of Linear Differenial Equaions In "Ordinary Differenial Equaions" we've learned how o solve a differenial equaion for a variable, such as: y'k5$e K2$x =0 solve DE yx = K 5 2 ek2 x C_C1 2$y''C7$y

More information

Chapter 15: Phenomena. Chapter 15 Chemical Kinetics. Reaction Rates. Reaction Rates R P. Reaction Rates. Rate Laws

Chapter 15: Phenomena. Chapter 15 Chemical Kinetics. Reaction Rates. Reaction Rates R P. Reaction Rates. Rate Laws Chaper 5: Phenomena Phenomena: The reacion (aq) + B(aq) C(aq) was sudied a wo differen emperaures (98 K and 35 K). For each emperaure he reacion was sared by puing differen concenraions of he 3 species

More information

2. For a one-point fixed time method, a pseudo-first order reaction obeys the equation 0.309

2. For a one-point fixed time method, a pseudo-first order reaction obeys the equation 0.309 Chaper 3. To derive an appropriae equaion we firs noe he following general relaionship beween he concenraion of A a ime, [A], he iniial concenraion of A, [A], and he concenraion of P a ime, [P] [ P] Subsiuing

More information

LAPLACE TRANSFORM AND TRANSFER FUNCTION

LAPLACE TRANSFORM AND TRANSFER FUNCTION CHBE320 LECTURE V LAPLACE TRANSFORM AND TRANSFER FUNCTION Professor Dae Ryook Yang Spring 2018 Dep. of Chemical and Biological Engineering 5-1 Road Map of he Lecure V Laplace Transform and Transfer funcions

More information

Solutions to Odd Number Exercises in Chapter 6

Solutions to Odd Number Exercises in Chapter 6 1 Soluions o Odd Number Exercises in 6.1 R y eˆ 1.7151 y 6.3 From eˆ ( T K) ˆ R 1 1 SST SST SST (1 R ) 55.36(1.7911) we have, ˆ 6.414 T K ( ) 6.5 y ye ye y e 1 1 Consider he erms e and xe b b x e y e b

More information

Basilio Bona ROBOTICA 03CFIOR 1

Basilio Bona ROBOTICA 03CFIOR 1 Indusrial Robos Kinemaics 1 Kinemaics and kinemaic funcions Kinemaics deals wih he sudy of four funcions (called kinemaic funcions or KFs) ha mahemaically ransform join variables ino caresian variables

More information

ME 391 Mechanical Engineering Analysis

ME 391 Mechanical Engineering Analysis Fall 04 ME 39 Mechanical Engineering Analsis Eam # Soluions Direcions: Open noes (including course web posings). No books, compuers, or phones. An calculaor is fair game. Problem Deermine he posiion of

More information

Chapter #1 EEE8013 EEE3001. Linear Controller Design and State Space Analysis

Chapter #1 EEE8013 EEE3001. Linear Controller Design and State Space Analysis Chaper EEE83 EEE3 Chaper # EEE83 EEE3 Linear Conroller Design and Sae Space Analysis Ordinary Differenial Equaions.... Inroducion.... Firs Order ODEs... 3. Second Order ODEs... 7 3. General Maerial...

More information

Sub Module 2.6. Measurement of transient temperature

Sub Module 2.6. Measurement of transient temperature Mechanical Measuremens Prof. S.P.Venkaeshan Sub Module 2.6 Measuremen of ransien emperaure Many processes of engineering relevance involve variaions wih respec o ime. The sysem properies like emperaure,

More information

Solutions to Assignment 1

Solutions to Assignment 1 MA 2326 Differenial Equaions Insrucor: Peronela Radu Friday, February 8, 203 Soluions o Assignmen. Find he general soluions of he following ODEs: (a) 2 x = an x Soluion: I is a separable equaion as we

More information

Matlab and Python programming: how to get started

Matlab and Python programming: how to get started Malab and Pyhon programming: how o ge sared Equipping readers he skills o wrie programs o explore complex sysems and discover ineresing paerns from big daa is one of he main goals of his book. In his chaper,

More information

dy dx = xey (a) y(0) = 2 (b) y(1) = 2.5 SOLUTION: See next page

dy dx = xey (a) y(0) = 2 (b) y(1) = 2.5 SOLUTION: See next page Assignmen 1 MATH 2270 SOLUTION Please wrie ou complee soluions for each of he following 6 problems (one more will sill be added). You may, of course, consul wih your classmaes, he exbook or oher resources,

More information

6.003 Homework 1. Problems. Due at the beginning of recitation on Wednesday, February 10, 2010.

6.003 Homework 1. Problems. Due at the beginning of recitation on Wednesday, February 10, 2010. 6.003 Homework Due a he beginning of reciaion on Wednesday, February 0, 200. Problems. Independen and Dependen Variables Assume ha he heigh of a waer wave is given by g(x v) where x is disance, v is velociy,

More information

Circuit Variables. AP 1.1 Use a product of ratios to convert two-thirds the speed of light from meters per second to miles per second: 1 ft 12 in

Circuit Variables. AP 1.1 Use a product of ratios to convert two-thirds the speed of light from meters per second to miles per second: 1 ft 12 in Circui Variables 1 Assessmen Problems AP 1.1 Use a produc of raios o conver wo-hirds he speed of ligh from meers per second o miles per second: ( ) 2 3 1 8 m 3 1 s 1 cm 1 m 1 in 2.54 cm 1 f 12 in 1 mile

More information

4.5 Constant Acceleration

4.5 Constant Acceleration 4.5 Consan Acceleraion v() v() = v 0 + a a() a a() = a v 0 Area = a (a) (b) Figure 4.8 Consan acceleraion: (a) velociy, (b) acceleraion When he x -componen of he velociy is a linear funcion (Figure 4.8(a)),

More information

A Bayesian Approach to Spectral Analysis

A Bayesian Approach to Spectral Analysis Chirped Signals A Bayesian Approach o Specral Analysis Chirped signals are oscillaing signals wih ime variable frequencies, usually wih a linear variaion of frequency wih ime. E.g. f() = A cos(ω + α 2

More information

8. Basic RL and RC Circuits

8. Basic RL and RC Circuits 8. Basic L and C Circuis This chaper deals wih he soluions of he responses of L and C circuis The analysis of C and L circuis leads o a linear differenial equaion This chaper covers he following opics

More information

ENEE 420 FALL 2010 COMMUNICATIONS SYSTEMS ANSWER KEY TO TEST # 2:

ENEE 420 FALL 2010 COMMUNICATIONS SYSTEMS ANSWER KEY TO TEST # 2: ENEE /FALL ENEE FALL COMMUNICAIONS SYSEMS ANSWER KEY O ES # :..a Fix in R. I is plain ha z = Φy AM = aa c + k A m cos πf c + ba c + k A m cos πf c = aa c + k A m cos πf c + b A c + k Am + cos πf c = aa

More information

u(x) = e x 2 y + 2 ) Integrate and solve for x (1 + x)y + y = cos x Answer: Divide both sides by 1 + x and solve for y. y = x y + cos x

u(x) = e x 2 y + 2 ) Integrate and solve for x (1 + x)y + y = cos x Answer: Divide both sides by 1 + x and solve for y. y = x y + cos x . 1 Mah 211 Homework #3 February 2, 2001 2.4.3. y + (2/x)y = (cos x)/x 2 Answer: Compare y + (2/x) y = (cos x)/x 2 wih y = a(x)x + f(x)and noe ha a(x) = 2/x. Consequenly, an inegraing facor is found wih

More information

Chapter 11. Heteroskedasticity The Nature of Heteroskedasticity. In Chapter 3 we introduced the linear model (11.1.1)

Chapter 11. Heteroskedasticity The Nature of Heteroskedasticity. In Chapter 3 we introduced the linear model (11.1.1) Chaper 11 Heeroskedasiciy 11.1 The Naure of Heeroskedasiciy In Chaper 3 we inroduced he linear model y = β+β x (11.1.1) 1 o explain household expendiure on food (y) as a funcion of household income (x).

More information

AASHTO Rigid Pavement Design

AASHTO Rigid Pavement Design AASHTO Rigid Pavemen Design Dr. Chrisos Drakos 1. Inroducion Empirical design based on he AASHO road es: Over 00 es secions JPCP (15 spacg) and JRPC (40 spacg) Range of slab hickness:.5 o 1.5 ches Subbase

More information

WEEK-3 Recitation PHYS 131. of the projectile s velocity remains constant throughout the motion, since the acceleration a x

WEEK-3 Recitation PHYS 131. of the projectile s velocity remains constant throughout the motion, since the acceleration a x WEEK-3 Reciaion PHYS 131 Ch. 3: FOC 1, 3, 4, 6, 14. Problems 9, 37, 41 & 71 and Ch. 4: FOC 1, 3, 5, 8. Problems 3, 5 & 16. Feb 8, 018 Ch. 3: FOC 1, 3, 4, 6, 14. 1. (a) The horizonal componen of he projecile

More information

6.003 Homework #9 Solutions

6.003 Homework #9 Solutions 6.00 Homework #9 Soluions Problems. Fourier varieies a. Deermine he Fourier series coefficiens of he following signal, which is periodic in 0. x () 0 0 a 0 5 a k sin πk 5 sin πk 5 πk for k 0 a k 0 πk j

More information

4.1.1 Mindlin plates: Bending theory and variational formulation

4.1.1 Mindlin plates: Bending theory and variational formulation Chaper 4 soropic fla shell elemens n his chaper, fia shell elemens are formulaed hrough he assembly of membrane and plae elemens. The exac soluion of a shell approximaed by fia faces compared o he exac

More information

Lecture 23 Damped Motion

Lecture 23 Damped Motion Differenial Equaions (MTH40) Lecure Daped Moion In he previous lecure, we discussed he free haronic oion ha assues no rearding forces acing on he oving ass. However No rearding forces acing on he oving

More information

2.4 Cuk converter example

2.4 Cuk converter example 2.4 Cuk converer example C 1 Cuk converer, wih ideal swich i 1 i v 1 2 1 2 C 2 v 2 Cuk converer: pracical realizaion using MOSFET and diode C 1 i 1 i v 1 2 Q 1 D 1 C 2 v 2 28 Analysis sraegy This converer

More information

Traveling Waves. Chapter Introduction

Traveling Waves. Chapter Introduction Chaper 4 Traveling Waves 4.1 Inroducion To dae, we have considered oscillaions, i.e., periodic, ofen harmonic, variaions of a physical characerisic of a sysem. The sysem a one ime is indisinguishable from

More information

ln 2 1 ln y x c y C x

ln 2 1 ln y x c y C x Lecure 14 Appendi B: Some sample problems from Boas Here are some soluions o he sample problems assigned for Chaper 8 8: 6 Soluion: We wan o find he soluion o he following firs order equaion using separaion

More information

d 1 = c 1 b 2 - b 1 c 2 d 2 = c 1 b 3 - b 1 c 3

d 1 = c 1 b 2 - b 1 c 2 d 2 = c 1 b 3 - b 1 c 3 and d = c b - b c c d = c b - b c c This process is coninued unil he nh row has been compleed. The complee array of coefficiens is riangular. Noe ha in developing he array an enire row may be divided or

More information

Week 1 Lecture 2 Problems 2, 5. What if something oscillates with no obvious spring? What is ω? (problem set problem)

Week 1 Lecture 2 Problems 2, 5. What if something oscillates with no obvious spring? What is ω? (problem set problem) Week 1 Lecure Problems, 5 Wha if somehing oscillaes wih no obvious spring? Wha is ω? (problem se problem) Sar wih Try and ge o SHM form E. Full beer can in lake, oscillaing F = m & = ge rearrange: F =

More information

Keywords: thermal stress; thermal fatigue; inverse analysis; heat conduction; regularization

Keywords: thermal stress; thermal fatigue; inverse analysis; heat conduction; regularization Proceedings Inverse Analysis for Esimaing Temperaure and Residual Sress Disribuions in a Pipe from Ouer Surface Temperaure Measuremen and Is Regularizaion Shiro Kubo * and Shoki Taguwa Deparmen of Mechanical

More information

AQA Maths M2. Topic Questions from Papers. Differential Equations. Answers

AQA Maths M2. Topic Questions from Papers. Differential Equations. Answers AQA Mahs M Topic Quesions from Papers Differenial Equaions Answers PhysicsAndMahsTuor.com Q Soluion Marks Toal Commens M 600 0 = A Applying Newonís second law wih 0 and. Correc equaion = 0 dm Separaing

More information

On Measuring Pro-Poor Growth. 1. On Various Ways of Measuring Pro-Poor Growth: A Short Review of the Literature

On Measuring Pro-Poor Growth. 1. On Various Ways of Measuring Pro-Poor Growth: A Short Review of the Literature On Measuring Pro-Poor Growh 1. On Various Ways of Measuring Pro-Poor Growh: A Shor eview of he Lieraure During he pas en years or so here have been various suggesions concerning he way one should check

More information

Navneet Saini, Mayank Goyal, Vishal Bansal (2013); Term Project AML310; Indian Institute of Technology Delhi

Navneet Saini, Mayank Goyal, Vishal Bansal (2013); Term Project AML310; Indian Institute of Technology Delhi Creep in Viscoelasic Subsances Numerical mehods o calculae he coefficiens of he Prony equaion using creep es daa and Herediary Inegrals Mehod Navnee Saini, Mayank Goyal, Vishal Bansal (23); Term Projec

More information

Shells with membrane behavior

Shells with membrane behavior Chaper 3 Shells wih membrane behavior In he presen Chaper he sress saic response of membrane shells will be addressed. In Secion 3.1 an inroducory example emphasizing he difference beween bending and membrane

More information

Vehicle Arrival Models : Headway

Vehicle Arrival Models : Headway Chaper 12 Vehicle Arrival Models : Headway 12.1 Inroducion Modelling arrival of vehicle a secion of road is an imporan sep in raffic flow modelling. I has imporan applicaion in raffic flow simulaion where

More information

In this chapter the model of free motion under gravity is extended to objects projected at an angle. When you have completed it, you should

In this chapter the model of free motion under gravity is extended to objects projected at an angle. When you have completed it, you should Cambridge Universiy Press 978--36-60033-7 Cambridge Inernaional AS and A Level Mahemaics: Mechanics Coursebook Excerp More Informaion Chaper The moion of projeciles In his chaper he model of free moion

More information

UNIVERSITY OF CALIFORNIA AT BERKELEY

UNIVERSITY OF CALIFORNIA AT BERKELEY Homework #10 Soluions EECS 40, Fall 2006 Prof. Chang-Hasnain Due a 6 pm in 240 Cory on Wednesday, 04/18/07 oal Poins: 100 Pu (1) your name and (2) discussion secion number on your homework. You need o

More information

Ch.1. Group Work Units. Continuum Mechanics Course (MMC) - ETSECCPB - UPC

Ch.1. Group Work Units. Continuum Mechanics Course (MMC) - ETSECCPB - UPC Ch.. Group Work Unis Coninuum Mechanics Course (MMC) - ETSECCPB - UPC Uni 2 Jusify wheher he following saemens are rue or false: a) Two sreamlines, corresponding o a same insan of ime, can never inersec

More information

R.#W.#Erickson# Department#of#Electrical,#Computer,#and#Energy#Engineering# University#of#Colorado,#Boulder#

R.#W.#Erickson# Department#of#Electrical,#Computer,#and#Energy#Engineering# University#of#Colorado,#Boulder# .#W.#Erickson# Deparmen#of#Elecrical,#Compuer,#and#Energy#Engineering# Universiy#of#Colorado,#Boulder# Chaper 2 Principles of Seady-Sae Converer Analysis 2.1. Inroducion 2.2. Inducor vol-second balance,

More information

SOLUTIONS TO ECE 3084

SOLUTIONS TO ECE 3084 SOLUTIONS TO ECE 384 PROBLEM 2.. For each sysem below, specify wheher or no i is: (i) memoryless; (ii) causal; (iii) inverible; (iv) linear; (v) ime invarian; Explain your reasoning. If he propery is no

More information

v A Since the axial rigidity k ij is defined by P/v A, we obtain Pa 3

v A Since the axial rigidity k ij is defined by P/v A, we obtain Pa 3 The The rd rd Inernaional Conference on on Design Engineering and Science, ICDES 14 Pilsen, Czech Pilsen, Republic, Czech Augus Republic, 1 Sepember 1-, 14 In-plane and Ou-of-plane Deflecion of J-shaped

More information

EECE 301 Signals & Systems Prof. Mark Fowler

EECE 301 Signals & Systems Prof. Mark Fowler EECE 3 Signals & Sysems Prof. Mark Fowler Noe Se #2 Wha are Coninuous-Time Signals??? Reading Assignmen: Secion. of Kamen and Heck /22 Course Flow Diagram The arrows here show concepual flow beween ideas.

More information

IV. Transport Phenomena. Lecture 19: Transient Diffusion. 1 Response to a Current Step. MIT Student. 1.1 Sand s Time

IV. Transport Phenomena. Lecture 19: Transient Diffusion. 1 Response to a Current Step. MIT Student. 1.1 Sand s Time IV. Transpor Phenomena Lecure 19: Transien iffusion MIT Suden In his lecure we show how o use simple scaling argumens o approximae he soluion o ransien diffusion problems, which arise in elecrochemical

More information

Non-uniform circular motion *

Non-uniform circular motion * OpenSax-CNX module: m14020 1 Non-uniform circular moion * Sunil Kumar Singh This work is produced by OpenSax-CNX and licensed under he Creaive Commons Aribuion License 2.0 Wha do we mean by non-uniform

More information

5.1 - Logarithms and Their Properties

5.1 - Logarithms and Their Properties Chaper 5 Logarihmic Funcions 5.1 - Logarihms and Their Properies Suppose ha a populaion grows according o he formula P 10, where P is he colony size a ime, in hours. When will he populaion be 2500? We

More information

Chapter 7: Solving Trig Equations

Chapter 7: Solving Trig Equations Haberman MTH Secion I: The Trigonomeric Funcions Chaper 7: Solving Trig Equaions Le s sar by solving a couple of equaions ha involve he sine funcion EXAMPLE a: Solve he equaion sin( ) The inverse funcions

More information

Math 334 Fall 2011 Homework 11 Solutions

Math 334 Fall 2011 Homework 11 Solutions Dec. 2, 2 Mah 334 Fall 2 Homework Soluions Basic Problem. Transform he following iniial value problem ino an iniial value problem for a sysem: u + p()u + q() u g(), u() u, u () v. () Soluion. Le v u. Then

More information

6.003: Signals and Systems. Relations among Fourier Representations

6.003: Signals and Systems. Relations among Fourier Representations 6.003: Signals and Sysems Relaions among Fourier Represenaions April 22, 200 Mid-erm Examinaion #3 W ednesday, April 28, 7:30-9:30pm. No reciaions on he day of he exam. Coverage: Lecures 20 Reciaions 20

More information

Explaining Total Factor Productivity. Ulrich Kohli University of Geneva December 2015

Explaining Total Factor Productivity. Ulrich Kohli University of Geneva December 2015 Explaining Toal Facor Produciviy Ulrich Kohli Universiy of Geneva December 2015 Needed: A Theory of Toal Facor Produciviy Edward C. Presco (1998) 2 1. Inroducion Toal Facor Produciviy (TFP) has become

More information

PET467E-Analysis of Well Pressure Tests/2008 Spring Semester/İTÜ Midterm Examination (Duration 3:00 hours) Solutions

PET467E-Analysis of Well Pressure Tests/2008 Spring Semester/İTÜ Midterm Examination (Duration 3:00 hours) Solutions M. Onur 03.04.008 PET467E-Analysis of Well Pressure Tess/008 Spring Semeser/İTÜ Miderm Examinaion (Duraion 3:00 hours) Soluions Name of he Suden: Insrucions: Before saring he exam, wrie your name clearly

More information

APPENDIX H FRACTURE PROPERTIES OF ASPHALT MIXTURES

APPENDIX H FRACTURE PROPERTIES OF ASPHALT MIXTURES APPENDIX H FRACTURE PROPERTIES OF ASPHALT MIXTURES LIST OF FIGURES Figure Page H- Loading ime under sress free emperaure... H-2 H-2 Mehod o evaluae he m mix of fracure properies for hermal case... H-3

More information

Simulation-Solving Dynamic Models ABE 5646 Week 2, Spring 2010

Simulation-Solving Dynamic Models ABE 5646 Week 2, Spring 2010 Simulaion-Solving Dynamic Models ABE 5646 Week 2, Spring 2010 Week Descripion Reading Maerial 2 Compuer Simulaion of Dynamic Models Finie Difference, coninuous saes, discree ime Simple Mehods Euler Trapezoid

More information

Chapter #1 EEE8013 EEE3001. Linear Controller Design and State Space Analysis

Chapter #1 EEE8013 EEE3001. Linear Controller Design and State Space Analysis Chaper EEE83 EEE3 Chaper # EEE83 EEE3 Linear Conroller Design and Sae Space Analysis Ordinary Differenial Equaions.... Inroducion.... Firs Order ODEs... 3. Second Order ODEs... 7 3. General Maerial...

More information

15. Vector Valued Functions

15. Vector Valued Functions 1. Vecor Valued Funcions Up o his poin, we have presened vecors wih consan componens, for example, 1, and,,4. However, we can allow he componens of a vecor o be funcions of a common variable. For example,

More information

Math 2142 Exam 1 Review Problems. x 2 + f (0) 3! for the 3rd Taylor polynomial at x = 0. To calculate the various quantities:

Math 2142 Exam 1 Review Problems. x 2 + f (0) 3! for the 3rd Taylor polynomial at x = 0. To calculate the various quantities: Mah 4 Eam Review Problems Problem. Calculae he 3rd Taylor polynomial for arcsin a =. Soluion. Le f() = arcsin. For his problem, we use he formula f() + f () + f ()! + f () 3! for he 3rd Taylor polynomial

More information

Lecture 20: Riccati Equations and Least Squares Feedback Control

Lecture 20: Riccati Equations and Least Squares Feedback Control 34-5 LINEAR SYSTEMS Lecure : Riccai Equaions and Leas Squares Feedback Conrol 5.6.4 Sae Feedback via Riccai Equaions A recursive approach in generaing he marix-valued funcion W ( ) equaion for i for he

More information

EECE 301 Signals & Systems Prof. Mark Fowler

EECE 301 Signals & Systems Prof. Mark Fowler EECE 31 Signals & Sysems Prof. Mark Fowler Noe Se #1 C-T Sysems: Convoluion Represenaion Reading Assignmen: Secion 2.6 of Kamen and Heck 1/11 Course Flow Diagram The arrows here show concepual flow beween

More information

Homework 4 (Stats 620, Winter 2017) Due Tuesday Feb 14, in class Questions are derived from problems in Stochastic Processes by S. Ross.

Homework 4 (Stats 620, Winter 2017) Due Tuesday Feb 14, in class Questions are derived from problems in Stochastic Processes by S. Ross. Homework 4 (Sas 62, Winer 217) Due Tuesday Feb 14, in class Quesions are derived from problems in Sochasic Processes by S. Ross. 1. Le A() and Y () denoe respecively he age and excess a. Find: (a) P{Y

More information

Differential Equations

Differential Equations Mah 21 (Fall 29) Differenial Equaions Soluion #3 1. Find he paricular soluion of he following differenial equaion by variaion of parameer (a) y + y = csc (b) 2 y + y y = ln, > Soluion: (a) The corresponding

More information

1 1 + x 2 dx. tan 1 (2) = ] ] x 3. Solution: Recall that the given integral is improper because. x 3. 1 x 3. dx = lim dx.

1 1 + x 2 dx. tan 1 (2) = ] ] x 3. Solution: Recall that the given integral is improper because. x 3. 1 x 3. dx = lim dx. . Use Simpson s rule wih n 4 o esimae an () +. Soluion: Since we are using 4 seps, 4 Thus we have [ ( ) f() + 4f + f() + 4f 3 [ + 4 4 6 5 + + 4 4 3 + ] 5 [ + 6 6 5 + + 6 3 + ]. 5. Our funcion is f() +.

More information

Hamilton- J acobi Equation: Weak S olution We continue the study of the Hamilton-Jacobi equation:

Hamilton- J acobi Equation: Weak S olution We continue the study of the Hamilton-Jacobi equation: M ah 5 7 Fall 9 L ecure O c. 4, 9 ) Hamilon- J acobi Equaion: Weak S oluion We coninue he sudy of he Hamilon-Jacobi equaion: We have shown ha u + H D u) = R n, ) ; u = g R n { = }. ). In general we canno

More information

Signal and System (Chapter 3. Continuous-Time Systems)

Signal and System (Chapter 3. Continuous-Time Systems) Signal and Sysem (Chaper 3. Coninuous-Time Sysems) Prof. Kwang-Chun Ho kwangho@hansung.ac.kr Tel: 0-760-453 Fax:0-760-4435 1 Dep. Elecronics and Informaion Eng. 1 Nodes, Branches, Loops A nework wih b

More information

T. J. HOLMES AND T. J. KEHOE INTERNATIONAL TRADE AND PAYMENTS THEORY FALL 2011 EXAMINATION

T. J. HOLMES AND T. J. KEHOE INTERNATIONAL TRADE AND PAYMENTS THEORY FALL 2011 EXAMINATION ECON 841 T. J. HOLMES AND T. J. KEHOE INTERNATIONAL TRADE AND PAYMENTS THEORY FALL 211 EXAMINATION This exam has wo pars. Each par has wo quesions. Please answer one of he wo quesions in each par for a

More information

CHEAPEST PMT ONLINE TEST SERIES AIIMS/NEET TOPPER PREPARE QUESTIONS

CHEAPEST PMT ONLINE TEST SERIES AIIMS/NEET TOPPER PREPARE QUESTIONS CHEAPEST PMT ONLINE TEST SERIES AIIMS/NEET TOPPER PREPARE QUESTIONS For more deails see las page or conac @aimaiims.in Physics Mock Tes Paper AIIMS/NEET 07 Physics 06 Saurday Augus 0 Uni es : Moion in

More information

Block Diagram of a DCS in 411

Block Diagram of a DCS in 411 Informaion source Forma A/D From oher sources Pulse modu. Muliplex Bandpass modu. X M h: channel impulse response m i g i s i Digial inpu Digial oupu iming and synchronizaion Digial baseband/ bandpass

More information

Suggested Problem Solutions Associated with Homework #5

Suggested Problem Solutions Associated with Homework #5 Suggesed Problem Soluions Associaed wih Homework #5 431 (a) 8 Si has proons and neurons (b) 85 3 Rb has 3 proons and 48 neurons (c) 5 Tl 81 has 81 proons and neurons 43 IDENTIFY and SET UP: The ex calculaes

More information

Robust estimation based on the first- and third-moment restrictions of the power transformation model

Robust estimation based on the first- and third-moment restrictions of the power transformation model h Inernaional Congress on Modelling and Simulaion, Adelaide, Ausralia, 6 December 3 www.mssanz.org.au/modsim3 Robus esimaion based on he firs- and hird-momen resricions of he power ransformaion Nawaa,

More information

Mechanical Fatigue and Load-Induced Aging of Loudspeaker Suspension. Wolfgang Klippel,

Mechanical Fatigue and Load-Induced Aging of Loudspeaker Suspension. Wolfgang Klippel, Mechanical Faigue and Load-Induced Aging of Loudspeaker Suspension Wolfgang Klippel, Insiue of Acousics and Speech Communicaion Dresden Universiy of Technology presened a he ALMA Symposium 2012, Las Vegas

More information