Statics and Strength of Materials
|
|
- Φιλύρη Παππάς
- 7 χρόνια πριν
- Προβολές:
Transcript
1 Instructor s Solutions Manual to accompany Statics and Strength of Materials Seventh Edition H.W. Morrow Robert P. Kokernak Upper Saddle River, New Jersey Columbus, Ohio
2 Copyright 2011, 2007, 2004, 2001, 1998, 1993 by Pearson Education, Inc., Upper Saddle River, New Jersey Pearson Prentice Hall. All rights reserved. Printed in the United States of America. This publication is protected by Copyright and permission should be obtained from the publisher prior to any prohibited reproduction, storage in a retrieval system, or transmission in any form or by any means, electronic, mechanical, photocopying, recording, or likewise. For information regarding permission(s), write to: Rights and Permissions Department. Pearson Prentice Hall is a trademark of Pearson Education, Inc. Pearson is a registered trademark of Pearson plc Prentice Hall is a registered trademark of Pearson Education, Inc. Instructors of classes using Morrow and Kokernak, Statics and Strength of Materials, 7/e, may reproduce material from the instructor s manual for classroom use ISBN-13: ISBN-10:
3 Contents Chapter 1 Basic Concepts 1 Chapter 2 Resultant of Concurrent Forces in a Plane 13 Chapter 3 Equilibrium of Concurrent Forces in a Plane 19 Chapter 4 Resultant of Nonconcurrent Forces in a Plane 23 Chapter 5 Equilibrium of a Rigid Body 29 Chapter 6 Force Analysis of Structures and Machines 41 Chapter 7 Forces in Space 77 Chapter 8 Friction 91 Chapter 9 Center of Gravity, Centroids, and Moments of Inertia of Areas 101 Chapter 10 Internal Reactions: Stress for Axial Loads 125 Chapter 11 Strain for Axial Loads: Hooke s Law 141 Chapter 12 Shear Stresses and Strains: Torsion 157 Chapter 13 Shear Forces and Bending Moments in Beams 167 Chapter 14 Bending and Shearing Stresses in Beams 179 Chapter 15 Deflection of Beams Due to Bending 205 Chapter 16 Combined Stresses and Mohr s Circle 235 Chapter 17 Columns 259 Chapter 18 Bolted, Riveted, and Welded Structural Connections 267
4 1 Basic Concepts 1. (a) 17.9 in. (25.40 mm)/1 in. = 455 mm = m < (b) 6.4 ft (304.8 mm)/1 ft = 1951 mm = m < (c) 13.8 in. (25.40 mm)/1 in. = 351 mm = m < (d) 95.2 ft (304.8 mm)/1 ft = mm = 29.0 m < 2. (a) 10.2 m (39.37 in.)/1 m = 402 in. = 33.5 ft < (b) 45.0 m (39.37 in.)/1 m = 1772 in. = ft < (c) 204 mm (39.37 in.)/1000 mm = 8.03 in. = ft < (d) 4600 mm (39.37 in.)/1000 mm = in. = ft < 3. 1 hr = 3600 s 1 mi = 5280 ft 60 mi 1 hr 5280 ft = 88.0 ft hr 3600 s 1 mi s < 4. (a) 60 W 1 hp W = hp < (b) 210 hp W 1 hp = W < 5. (a) 23.5 lb (4.448 N)/1 lb = N = kn < (b) 5.8 kips (4448 N)/1 kip = N = 25.8 kn < (c) 250 lb (4.448 N)/1 lb = 1112 N = kn < (d) 15.9 kips (4448 N)/1 kip = N = 70.7 kn < 6. (a) 52.9 N ( lb)/1 N = lb = kip < (b) 6.85 kn (224.8 lb)/1 kn = 1540 lb = kips < 7. (a) 250 kg 9.81 m/s 2 = 2450 N = 2.45 kn < (b) 4.5 Mg: kg 9.81 m/s 2 = N = 44.1 kn < (c) m/s 2 = 3680 N = 3.68 kn < (d) 25.0 Mg: kg 9.81 m/s 2 = N = 245 kn < (e) kg: 140 kg 9.81 m/s 2 = 1373 N = kn < 8. (a) 2000 N/9.81 m/s 2 = 204 kg < (b) 3.50 kn: 3500 N/9.81 m/s 2 = 357 kg < (c) 1200 N/9.81 m/s 2 = kg < (d) 4.40 kn: 4400 N/9.81 m/s 2 = 449 kg < 9. (a) lb/ft 3 (1 ft/0.3048) 3 (4.448 N/lb) = 9810 N/m 3 = 9.81 kn/m 3 < (b) lb ft 3 1 ft in in gal 55 gal = 459 lb < (10 in. 22 in.) (1 ft 2 /144 in. 2 ) = 229 lb/ft < (229 lb/ft)(1 ft/ m)(4.448 N/lb) = 3344 N/m = 3.34 kn/m < (3344 N/m)(1 kg/9.81 N) = 341 kg/m < 11. (1 lb/in. 2 )(4.448 N/lb) (1 in./ m) 2 = 6894 N/m 2 = 6.89 kpa(kn/m 2 ) < [(6894 N/m 2 )/(1 lb/in. 2 )] (14.7 lb/in. 2 ) = Pa = kpa(kn/m 2 ) < Chapter 1 1
5 MN/m 2 = N/m 2 ( N/m 2 )(1 lb/4.448 N) (1 m/39.37 in.) 2 = lb/in. 2 (psi) < = 36.3 kips/in. 2 (ksi) < 55 MN/m 2 = N/m 2 ( N/m 2 )(1 lb/4.448 N) (1 m/39.37 in.) 2 < = lb/in. 2 (psi) = 7.98 kips/in. 2 (ksi) < ,560 ft 2 ( m/ft) 2 = 4050 m 2 < MN/m 2 = N/m N/m 2 (1 lb/4.448 N) (1 m/39.37 in.) 2 = lb/in. 2 (psi) < = 58.0 kips/in. 2 (ksi) < N/m 2 (1 lb/4.448 N) (1 m/39.37 in.) 2 = lb/in. 2 (psi) < = kips/in. 2 (ksi) < 15. (a) c 2 = (475) 2 + (950) 2 c = 1062 mm < θ = arctan (475/950) = 26.6 sin 26.6 = < cos 26.6 = < (b) c 2 = , c = 10 ft sin θ = (6/10) = 0.6 < cos θ = (8/10) = 0.8 < 16. (a) d = cos 70 = m d = 8 m = 2.74 m < (b) h = sin 70 = m h = 8 m = 7.52 m < CHECK: d 2 + h 2 = (8 m) 2? 17. θ 1 = 45, θ 2 = 35, d = 300 mm Eliminating b from the two Eq. (a) of Prob. 1.16, we have (c + d)/tan θ 1 = d/tan θ 2 c = d(tan θ 1 tan θ 2 )/ tan θ 2 = 300(tan 45 tan 35 )/ tan 35 c = m < From Eq. (a), we have b = (c + d)/ tan θ 1 = ( )/tan 45 = 428 m < 18. b = 10 ft = 120 in. h = 5 ft 8 in. = 68 in. tan θ = h/b = 68/120; θ = 29.5 < 19. tan 28 = h/40 h = 40 tan 28 h = 21.3 m < Chapter 1 2
6 20. tan 22 = 288/b b = 288/tan 22 = = 713 ft < 21. h 2 = 30 tan 42 = 27.0 m < h 1 = 124 h 2 = = 97.0 m < 22. Distance AE = BC = 200 ft Distance ED = 340 ft 225 ft = 115 ft Then for triangle AED: (AD) 2 = (200 ft) 2 + (115 ft) 2 AD = Road frontage = ft < 23. In triangle ABD: AD = sin 54 or AD = m 6.0 m BD 6.0 m = cos 54 or BD = m In triangle ACD: (CD) 2 + (4.854 m) 2 = (8.0 m) 2 CD = m Then: x = BC = CD BD x = m m x = m < 24. (AC) 2 = (14 in.) 2 + (14 in.) 2 AC = 19.8 in. AB = BC = 1 (80 in in.) 2 AB = BC = 26 in. 9.8 in. sin θ = = in. θ = Angle ABC = 2θ = 44.3 < Chapter 1 3
7 25. Using bracket dimensions: (AC) 2 = (2.5 m) 2 + (0.6 m) 2 AC = 2.57 m tan β = 2.5 m = β = m α = = 55 θ = 180 α β = 48.5 In triangle ABC: AB = sin θ AC AB 2.57 m AB = 1.93 m < = sin (a) In triangle ECG, let angle CEG = θ. Then: CG tan θ = 16 ft = EG (8 ft + 8 ft) So: θ = 45 Similarly, the following angles are equal to θ: BAH, BGH, DGF, ABH, GBH, BCG, FDG, EDF, and DCG. (b) In triangle DEF, DF = tan 95 = EF so DF = BH = 8 ft and (DE) 2 = (8 ft) 2 + (8 ft) 2 or DE = ft = DG = BG = AB Since angle CDG = 90, then CD = DG = CB = BG = ft Total lineal feet: 8 ft) ft) + 16 ft) = 132 ft < 27. From the Fig. tan 37 = h/b tan 56 = (400 + h)/b (a) (b) Eliminating b beween Eqs. (a) and (b), we have h/tan 37 = (400 + h)/tan 56 or h(tan 56 tan 37 ) = 400 tan 37 h = 400 tan 37 /(tan 56 tan 37 ) h = = 414 m 28. (a) For Fig. a = 7 in., B = 40, C = 30 A = 180 B C = 110 From Fig. and law of sines b/sin 40 = c/sin 30 = 7/sin 110 b = 7 sin 40 /sin 110 = 4.79 in. < c = 7 sin 30 /sin 110 = 3.72 in. < (b) a = 3 m, b = 6 m, C = 48 From Fig. and law of cosines c 2 = (6) 2 + (3) 2 2(6)(3) cos 48 c = 4.57 m < From Fig. and law of sines sin A/3 = sin 48 /4.57 sin A = ; A = 29.2 < B = 180 A C; B = < Chapter 1 4
8 (c) a = 8 ft, b = 7 ft, A = 60 From Fig. and law of sines sin B/7 = sin 60 /8 sin B = ; B = 49.3 < C = 180 A B; C = 70.7 < From Fig. and law of cosines c 2 = (7) 2 + (8) 2 2(7)(8) cos 70.7 c = 8.72 ft < (d) a = 4 m, b = 7 m, c = 9 m From Fig. and law of cosines (9) 2 = (7) 2 + (4) 2 2(7)(4) cos C cos C = ; C = < & (4) 2 = (7) 2 + (9) 2 2(7)(9) cos A cos A = ; A = 25.2 < B = 180 A C; B = 48.2 < 29. (a) 8 in., 12.5 in., 65 From Fig. and law of cosines (AC) 2 = (8) 2 + (12.5) 2 2(8)(12.5) cos( ); AC = in. < (BD) 2 = (8) 2 + (12.5) 2 2(8)(12.5) cos 65 ; BD = in. < (b) 550 mm, 320 mm, 55 From Fig. and law of cosines (AC) 2 = (550) 2 + (320) 2 2(550)(320) cos( ); AC = 779 mm < (BD) 2 = (550) 2 + (320) 2 2(550)(320) cos 55 ; BD = 451 mm < (c) 10.3 ft, 12.5 ft, 45 From Fig. and law of cosines (AC) 2 = (10.3) 2 + (12.5) 2 2(10.3)(12.5) cos( ) AC = 21.1 ft < (BD) 2 = (10.3) 2 + (12.5) 2 2(10.3)(12.5) cos 45 BD = 8.96 ft < (d) 5 m, 12 m, 125 From Fig. and law of cosines (AC) 2 = (5) 2 + (12) 2 2(5)(12) cos( ); AC = m < (BD) 2 = (5) 2 + (12) 2 2(5)(12) cos 125 ; BD = m < 30. From Fig. and the law of cosines (AB) 2 = (5) 2 + (8) 2 2(5)(8) cos 40 AB = 5.26 ft < From Fig. and law of sines sin A/8 = sin 40 /5.26 sin A = A = = θ = A 90 = = < Chapter 1 5
9 31. From Fig. and law of cosines (BC) 2 = (28.3) 2 + (44.7) 2 2(28.3)(44.7) cos 18.4 BC = ft < From Fig. and law of sines sin BCD/28.3 = sin DBC/44.7 = sin 18.4 /19.96 sin BCD = ; BCD = 26.6 < sin DBC = DBC = = < DBA = = 45 < AD = AB tan ABD = AC tan BCD AB tan 45 = (AB ) tan 26.6 AB = ft AC = = 40.0 ft < 32. OA = 120 mm, AB = 300 mm From the law of sines sin 35 /300 = sin A/OB = sin B/120 sin B = (120/300) sin 35 Angle B = Angle A = = OB = 300 sin A/sin 35 = 300 sin /sin 35 OB = 390 mm < (120) 2 + (OB ) 2 = (300) 2 OB = 275 mm < Distance moved = OB OB = = mm < 33. Fig. (1) (a) From Fig. (1) tan θ 1 = 1.5/6; θ 1 = tan θ 2 = ( )/6; θ 2 = and GCB = 90 θ 2 = = 76.0 < Chapter 1 6
10 (b) From Fig. (2) JK = 1.5 tan θ 2 = m KA = 2 JK = m tan θ 3 = 1.125/1.5 θ 3 = AHJ = θ 1 + θ 2 = 67.1 < Fig. (2) 34. From the Fig. tan θ 1 = 3/36 θ 1 = 4.76 BAH = 90 θ 1 = 85.2 < (AD) 2 = (3) 2 + (36) 2 AD = BC = AD/3 = ft BAH = CBG From Fig. and law of cosines (CG) 2 = (18) 2 + (12.04) 2 2(18)(12.04) cos 85.2 CG = ft From the figure of the tower and the law of sines sin BCG sin 85.2 = sin BCG = BCG = 59.5 < DEF = 90 + θ 1 = 94.8 < 35. (a) Law of sines: 9.15 m = 5.50 m sin 65 sin α α = 33.0 β = α = 82.0 So 9.15 m = h sin 65 sin 82.0 h = 10.0 m < (b) Law of sines: 13.7 m = 10.0 m sin 115 sin θ θ = 41.4 γ = θ = m = dd sin 115 sin 23.6 d = 6.05 m < 36. In triangle ABD, law of sines yields: dd = 75 ft sin 138 sin 14 d = ft In right triangle ACD: h = sin 28 = ft h = 97.4 ft, tree will hit house < Chapter 1 7
11 37. (a) Law of sines: 225 ft = WW sin 130 sin 30 W = ft < (b) h = (225 ft)sin 20 = 77.0 ft V = ft (146.9 ft)(77.0 ft)( ) 2 8 = 3,732,729 ft 3 1 cu. yd. V = 3,732,729 ft 3 27 ft 3 V = 138,249 cu. yds. < 138,249 cu. yds. (c) No. of truckloads = 20 cu. yds./truck = 6,912 truckloads < 38. From law of cosines: R 2 = (18) 2 + (32) 2 2(18)(32) cos 41.5 R = 22.0 ft < From law of sines: 18 ft sin B = 22.0 ft sin 41.5 sin B = B = 32.8 < 39. From law of cosines: (14) 2 = r 2 + r 2 2(r)(r) cos 120 r = 8.08 cm d = 2r = 16.2 cm < DD = = 15(3) 21( 2) 2 3 = DDDD = = 12(3) (21)(17) 17 3 = DDDD = = 15(17) (12)( 2) 2 17 = 231 Dividing Dx and Dy by D, we have xx = 321 = 107, yy = 231 = 77 < DD = = 19( 21) ( 20)(20) = DDDD = = ( 22)( 21) ( 20)( 23) = Chapter 1 8
12 DDDD = = 19( 23) ( 22)(20) = Dividing Du and Dv by D, we have uu = 2 = 2, vv = 3 = 3 < DD = 5 3 = 5( 5) ( 3)(3) 3 5 = DDDD = = 9( 5) ( 3)( 9) = DDDD = 5 9 = 5( 9) 9(3) = Dividing Dm and Dn by D, we have mm = = 4.5, nn = = 4.5 < DD = 2 2 = (2)( 1) (1)(2) = DDDD = = (3)( 1) ( 0.9)(2) = DDDD = 2 3 = (2)( 0.9) (1)(3) = Then: AA = DDDD DD 4 = 0.3 < BB = DDDD DD 4 = 1.2 < 45. 7x + 10y = 10 < 9x 5y = 5 < xx = = ( 50) ( 50) 9 5 (35) (90) = 0 55 = 0 < yy = = (35) (90) 9 5 (35) (90) Equation set is valid. = = +1 < Chapter 1 9
13 46. $10.10 = F + 12r < $13.95 = F +19r < FF = = (191.90) (167.40) 1 19 (19) (12) F = $3.50 < rr = = (13.95) (10.10) 1 19 (19) (12) r = $0.55/lb < 47. C = Cost of one 2 4 P = Cost of one C + 200P = $ < 140C + 125P = $ < CC = = 29, ,750 C = $1.85 < ,750 PP = P = $2.15 < = 33, , (1 st column) DD = = 2[1(2) 1( 3)] 1[3(2) ( 2)( 3)] + ( 1)[3(1) ( 2)(1)] = (2 nd row) DDDD = = 2[3(2) ( 2)( 3)] + 1[( 7)(2) ( 2)(5)] 1[( 7)( 3) (3)(5)] = 10 (1st column) DDDD = = 2[2(2) 1(5)] 1[( 7)(2) ( 2)(5)] + ( 1)[( 7)(1) ( 2)(2)] = (1st column) DDDD = = 2[1(5) 2( 3)] 1[3(5) ( 7)( 3)] + ( 1)[3(2) ( 7)(1)] = Dividing Dx, Dy, & Dz by D, we have xx = 10 5 = 2, yy = 5 5 = 1, zz = 15 5 = 3 < DD = = +(1)( 2)(1) + (3)(3)( 1) + (2)( 2)(1) (2)( 2)( 1) (1)(3)(1) (3)( 2)(1) = 16 Chapter 1 10
14 DDDD = = +(2)( 2)(1) + (3)(3)( 1) + (2)(1)(1) (2)( 2)( 1) (2)(3)(1) (3)(1)(1) = DDDD = = +(1)(1)(1) + (2)(3)( 1) + (2)( 2)( 1) (2)(1)( 1) (1)(3)( 1) (2)( 2)(1) = DDDD = = +(1)( 2)( 1) + (3)(1)( 1) + (2)( 2)(1) (2)( 2)( 1) (1)(1)(1) (3)( 2)( 1) = 16 Dividing DP, DQ, & DR by D, we have P = 24 = 1.5, 16 QQ = 8 16 = 0.5, RR = = 1 < DD = = +(0)(2)(1) + (1)( 1)(3) + (2)( 2)( 1) (2)(2)(3) (0)( 1)( 1) (1)( 2)(1) = DDDD = = +(1)(2)(1) + (1)( 1)(2) + (2)(3)( 1) (2)(2)(2) (1)( 1)( 1) (1)(3)(1) = DDDD = = +(0)(3)(1) + (1)( 1)(3) + (2)( 2)(2) (2)(3)(3) (0)( 1)(2) (1)( 2)(1) = DDDD = = +(0)(2)(2) + (1)(3)(3) + (1)( 2)( 1) (1)(2)(3) (0)(3)( 1) (1)( 2)(2) = 9 Dividing Dx, Dy, & Dz by D, we have xx = = 2, yy = = 3, zz = 9 = 1 < DD = = +(2)(1)(1) + (3)( 4)(1) + (2)(2)(2) (2)(1)(1) (2)( 4)(2) (3)(2)(1) = 6 Chapter 1 11
15 DDDD = = +(3)(1)(1) + (3)( 4)(2) + (2)(4)(2) (2)(1)(2) (3)( 4)(2) (3)(4)(1) = DDDD = = +(2)(4)(1) + (3)( 4)(1) + (2)(2)(2) (2)(4)(1) (2)( 4)(2) (3)(2)(1) = DDDD = = +(2)(1)(2) + (3)(4)(1) + (3)(2)(2) (3)(1)(1) Dividing DA, DB, & DC by D, we have A = 3 = 0.5, BB = 6 3 = 1, CC = = 0.5 < L = Lightest casting weight M = Middle casting weight H = Heaviest casting weight L + M + H = 1867 < H L = 395 < 2L = M + H 427 < Aligning equations: L + M + H = 1867 < L + H = 395 < 2L M H = 427 < LL = MM = HH = = = = (2)(4)(2) (3)(2)(2) = 3 = 480 lb < = 512 lb < = 875 lb < Chapter 1 12
16 2 Resultant of Concurrent Forces in a Plane R = < R = < 3. R 2 = (2.0) 2 + (1.5) 2 2(2.0)(1.5) cos 100 R = 2.70 kips (sin B/1.5) = (sin 100 /2.70) B = 33.2 θ = 35 + B = 68.2 R = < 4. R 2 = (6.0) 2 + (8.5) 2 2(6.0)(8.5) cos 105 R = kn (sin A/8.5) = (sin 105 /11.60) A = 45.1 θ = 35 + A = 80.1 R = < 5. R 2 = (300) 2 + (525) 2 2(300)(525) cos 110 R = lb (sin B/525) = (sin 110 /688.0) B = θ = B 45 = 0.81 R = < Chapter 2 13
17 6. A = = 25 (R/sin 110 ) = (Q/sin 45 ) = (24/sin 25 ) R = 53.4 kn < Q = 40.2 kn < 7. Q 2 = (15) 2 + (35) 2 2(15)(35) cos 30 Q = 23.3 kips < (sin θ 2 )/15 = (sin 30 )/23.3 θ 2 = 18.8 < 8. C = = 115 Q/sin 40 = P/sin 25 = 14/sin 115 Q = 9.93 kn < P = 6.53 kn < 9. (R ) 2 = (800) 2 + (600) 2 2(800)(600) cos 120 R = N N = 600 N θ = 25.3 sin 120 sin θ 10. (R) 2 = (1216.6) 2 + (400) 2 2(1216.6)(400) cos ( ) R = 1434 N 1434 N = 400 N α = 14.6 sin sin α R = 1434 (30 + θ + α) R = < 11. R = < R = < Chapter 2 14
18 12. R = < 13. Direction: right or up is + P = P cos θ, P = P sin θ (a) : kn, kn < (b) : kn, kn < 14. Direction: right or up is + P = P cos θ, P = P sin θ (a) : lb, lb < (b) : lb, lb < 15. Direction: right or up is + F x = F cos θ, F y = F sin θ (a) 22.9 kn, kn < (b) lb, +388 lb < (c) 2.64 kips, kips < (d) 289 N, 345 N < 16. Direction: right or up is + FF xx = FF cos θ, FF yy = FF sin θ (a) : 27.6 kn, kn < (b) : lb, 750 lb < (c) : kips, kips < (d) : 448 N, 39.2 N < 17. Perpendicular component: FF1 = cos 34 = N F1 = N < Parallel component: FF2 = sin 34 = N F2 = N < Chapter 2 15
19 14 in. 18. tan α = = in. α = 28.3 tan β = (14 in in.) 26 in. = β = 63.4 θ = β α = 35.1 Parallel component: F1 = 1650 lb cos 35.1 = 1350 lb < Perpendicular component: F2 = 1650 lb sin 35.1 = lb < 19. R x = FF xx = 3.4 cos cos 243 R x = kips R y = FF yy = 3.4 sin sin 243 R y = kips R 2 = ( 4.365) 2 + ( 1.672) 2 R = 4.67 kip < tan θ = = θ = ~ 21.0 in 3 rd quadrant or θ = 201 < 20. R x = FF xx R x = 12.5 cos cos 105 = 7.85 kn R y = FF yy = 12.5 sin sin 105 = kn R 2 = (7.85) 2 + (17.36) 2 = R = kn < θ = arctan (17.36/7.85) θ = < 21. FF xx = 2.15 cos 115 R x = kn FF yy = 2.15 sin sin ( 90 ) R y = kn R 2 = ( 0.909) 2 + ( 1.511) 2 R = 1.76 kn < θ 1 = arctan ( 1.511/ 0.909) = 59.0 θ = = 121 < 22. FF xx = (3/ 13) R x = kips FF yy = 3.81(2/ 13) 3.65 R y = kips R 2 = ( 7.900) 2 + ( 1.537) 2 R = 8.05 kips < θ 1 = arctan ( 1.537/ 7.900) = 11.0 θ = = 169 < 23. R x = FF xx = 0 FF xx = S x cos cos 140 = 0 S x = 83.3 N R y = FF yy = 500 FF yy = S y sin sin 140 = 500, S y = N S 2 = (83.3) 2 + (355.2) 2 ; S = 365 N < Chapter 2 16
20 θ = arctan (355.2/83.3) = < 24. R x = FF xx = 4800 FF xx = V x cos cos 45 V x = 2616 lb R y = FF yy = 0 FF yy = 1000 sin sin 10 + V y = 0 V y = lb V 2 = (2616) 2 + (967.6) 2 V = 2790 lb < θ = arctan ( 967.6/2616) = 20.3 < 25. Solve Prob. 2.1 by components. R x = FF xx = 20 cos cos 65 = 30.1 lb R y = FF yy = 20 sin sin 65 = lb R 2 = (30.1) 2 + (18.87) 2 R = 35.5 lb < θ = arctan ( 18.87/30.1) = 32.1 < 26. Solve Prob. 2.2 by components. R x = FF xx = 80 cos cos 110 = 53.7 N R y = FF yy = 80 sin sin 110 = 85.5 N R 2 = (53.7) 2 + (85.5) 2 R = N < θ = arctan ( 85.5/53.7) = 57.9 < 27. Solve Prob. 2.3 by components. R x = FF xx = 1.5 cos cos 145 = kips R y = FF yy = 1.5 sin sin 145 = 2.51 kips R 2 = (1.004) 2 + (2.70) 2 R = 2.70 kips < θ 1 = arctan (2.51/ 1.004) = 68.2 θ = = < 28. Solve Prob. 2.4 by components. R x = FF xx = 6.0 cos cos 110 = 2.01 kn R y = FF yy = 6.0 sin sin 110 = kn R 2 = (2.01) 2 + (11.43) 2 R = kn < θ = arctan (11.43/2.01) = < 29. Solve Prob. 2.9 by components. R x = FF xx = 30 cos cos cos 120 = 54.7 kn R y = FF yy = sin sin sin 120 = kn R 2 = (54.7) 2 + (15.34) 2 R = 56.8 kn < θ 1 = arctan (15.34/ 54.7) = 15.7 θ = = < 30. Solve Prob by components. R x = FF xx = 8 cos cos cos 110 = kips R y = FF yy = sin sin sin 110 = 7.62 kips R 2 = (10.81) 2 + (7.62) 2 Chapter 2 17
21 R = kips < θ = arctan ( 7.62/10.81) = 35.2 < 31. Solve Prob by components. R x = FF xx = cos cos 120 = 352 lb R y = FF yy = 180 sin sin sin 90 = lb R 2 = (352) 2 + (17.18) 2 R = 352 lb < θ = arctan (17.18/352) = < 32. Solve Prob by components. R x = FF xx = cos cos 120 = 7.83 kips R y = FF yy = 4.0 sin sin sin 90 = 3.22 kips R 2 = (7.83) 2 + (3.22) 2 R = 8.47 kips < θ = arctan (3.22/7.83) = < 33. Find F 1 F 2 Prob by comp. R x = FF xx = 3.0 cos cos 140 = kips R y = FF yy = 3.0 sin sin 140 = 4.33 kips R 2 = (0.647) 2 + (4.33) 2 R = 4.37 kips θ 1 = arctan (4.33/ 0.647) = 81.6 < θ = = < 34. Find P Q Prob by comp. R x = FF xx = 11.5 cos cos 150 = kn R y = FF yy = 11.5 sin sin 150 = 4.86 kn R 2 = (13.80) 2 + (4.86) 2 R = kn < θ 1 = arctan (4.86/ 13.80) = 19.4 θ = = < 35. FF xx = 1.65 cos cos 90 = kn FF yy = 1.65 sin sin 90 = kn Q = 1.92 kn R 2 = (0.697) 2 + (3.415) 2 ; R = 3.49 kn < θ = arctan ( 3.415/0.697) = 78.5 < 36. FF xx = 4.5 cos ( 3/13) = 7.50 kips FF yy = 3.5 sin (2/13) = 5.50 kips R 2 = (7.50) 2 + (5.50) 2 ; R = 9.30 kips < θ 1 = arctan (5.50/ 7.50) = 36.3 θ = = < Chapter 2 18
Chapter 7 Transformations of Stress and Strain
Chapter 7 Transformations of Stress and Strain INTRODUCTION Transformation of Plane Stress Mohr s Circle for Plane Stress Application of Mohr s Circle to 3D Analsis 90 60 60 0 0 50 90 Introduction 7-1
Matrices and Determinants
Matrices and Determinants SUBJECTIVE PROBLEMS: Q 1. For what value of k do the following system of equations possess a non-trivial (i.e., not all zero) solution over the set of rationals Q? x + ky + 3z
Homework 8 Model Solution Section
MATH 004 Homework Solution Homework 8 Model Solution Section 14.5 14.6. 14.5. Use the Chain Rule to find dz where z cosx + 4y), x 5t 4, y 1 t. dz dx + dy y sinx + 4y)0t + 4) sinx + 4y) 1t ) 0t + 4t ) sinx
Section 8.3 Trigonometric Equations
99 Section 8. Trigonometric Equations Objective 1: Solve Equations Involving One Trigonometric Function. In this section and the next, we will exple how to solving equations involving trigonometric functions.
ADVANCED STRUCTURAL MECHANICS
VSB TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING ADVANCED STRUCTURAL MECHANICS Lecture 1 Jiří Brožovský Office: LP H 406/3 Phone: 597 321 321 E-mail: jiri.brozovsky@vsb.cz WWW: http://fast10.vsb.cz/brozovsky/
Parts Manual. Trio Mobile Surgery Platform. Model 1033
Trio Mobile Surgery Platform Model 1033 Parts Manual For parts or technical assistance: Pour pièces de service ou assistance technique : Für Teile oder technische Unterstützung Anruf: Voor delen of technische
CRASH COURSE IN PRECALCULUS
CRASH COURSE IN PRECALCULUS Shiah-Sen Wang The graphs are prepared by Chien-Lun Lai Based on : Precalculus: Mathematics for Calculus by J. Stuwart, L. Redin & S. Watson, 6th edition, 01, Brooks/Cole Chapter
Areas and Lengths in Polar Coordinates
Kiryl Tsishchanka Areas and Lengths in Polar Coordinates In this section we develop the formula for the area of a region whose boundary is given by a polar equation. We need to use the formula for the
Macromechanics of a Laminate. Textbook: Mechanics of Composite Materials Author: Autar Kaw
Macromechanics of a Laminate Tetboo: Mechanics of Composite Materials Author: Autar Kaw Figure 4.1 Fiber Direction θ z CHAPTER OJECTIVES Understand the code for laminate stacing sequence Develop relationships
Κλινικοί Εκπαιδευτές: σύντομη περιγραφή ρόλου, κριτήρια επιλογής & πρόγραμμα εκπαίδευσης
σύντομη περιγραφή ρόλου, κριτήρια επιλογής & πρόγραμμα εκπαίδευσης 1 Σεπτέμβριος 2012 2012 4 η ΥΠΕ. Με επιφύλαξη παντός δικαιώματος. Απαγορεύεται αναδημοσίευση της έκδοσης σε οποιαδήποτε μορφή, ολόκληρης
CHAPTER 25 SOLVING EQUATIONS BY ITERATIVE METHODS
CHAPTER 5 SOLVING EQUATIONS BY ITERATIVE METHODS EXERCISE 104 Page 8 1. Find the positive root of the equation x + 3x 5 = 0, correct to 3 significant figures, using the method of bisection. Let f(x) =
1 Adda247 No. 1 APP for Banking & SSC Preparation Website:store.adda247.com
Adda47 No. APP for Banking & SSC Preparation Website:store.adda47.com Email:ebooks@adda47.com S. Ans.(d) Given, x + x = 5 3x x + 5x = 3x x [(x + x ) 5] 3 (x + ) 5 = 3 0 5 = 3 5 x S. Ans.(c) (a + a ) =
Trigonometric Formula Sheet
Trigonometric Formula Sheet Definition of the Trig Functions Right Triangle Definition Assume that: 0 < θ < or 0 < θ < 90 Unit Circle Definition Assume θ can be any angle. y x, y hypotenuse opposite θ
Section 7.6 Double and Half Angle Formulas
09 Section 7. Double and Half Angle Fmulas To derive the double-angles fmulas, we will use the sum of two angles fmulas that we developed in the last section. We will let α θ and β θ: cos(θ) cos(θ + θ)
Math221: HW# 1 solutions
Math: HW# solutions Andy Royston October, 5 7.5.7, 3 rd Ed. We have a n = b n = a = fxdx = xdx =, x cos nxdx = x sin nx n sin nxdx n = cos nx n = n n, x sin nxdx = x cos nx n + cos nxdx n cos n = + sin
Areas and Lengths in Polar Coordinates
Kiryl Tsishchanka Areas and Lengths in Polar Coordinates In this section we develop the formula for the area of a region whose boundary is given by a polar equation. We need to use the formula for the
Mock Exam 7. 1 Hong Kong Educational Publishing Company. Section A 1. Reference: HKDSE Math M Q2 (a) (1 + kx) n 1M + 1A = (1) =
Mock Eam 7 Mock Eam 7 Section A. Reference: HKDSE Math M 0 Q (a) ( + k) n nn ( )( k) + nk ( ) + + nn ( ) k + nk + + + A nk... () nn ( ) k... () From (), k...() n Substituting () into (), nn ( ) n 76n 76n
If we restrict the domain of y = sin x to [ π, π ], the restrict function. y = sin x, π 2 x π 2
Chapter 3. Analytic Trigonometry 3.1 The inverse sine, cosine, and tangent functions 1. Review: Inverse function (1) f 1 (f(x)) = x for every x in the domain of f and f(f 1 (x)) = x for every x in the
If we restrict the domain of y = sin x to [ π 2, π 2
Chapter 3. Analytic Trigonometry 3.1 The inverse sine, cosine, and tangent functions 1. Review: Inverse function (1) f 1 (f(x)) = x for every x in the domain of f and f(f 1 (x)) = x for every x in the
Reminders: linear functions
Reminders: linear functions Let U and V be vector spaces over the same field F. Definition A function f : U V is linear if for every u 1, u 2 U, f (u 1 + u 2 ) = f (u 1 ) + f (u 2 ), and for every u U
Review Exercises for Chapter 7
8 Chapter 7 Integration Techniques, L Hôpital s Rule, and Improper Integrals 8. For n, I d b For n >, I n n u n, du n n d, dv (a) d b 6 b 6 (b) (c) n d 5 d b n n b n n n d, v d 6 5 5 6 d 5 5 b d 6. b 6
3.4 SUM AND DIFFERENCE FORMULAS. NOTE: cos(α+β) cos α + cos β cos(α-β) cos α -cos β
3.4 SUM AND DIFFERENCE FORMULAS Page Theorem cos(αβ cos α cos β -sin α cos(α-β cos α cos β sin α NOTE: cos(αβ cos α cos β cos(α-β cos α -cos β Proof of cos(α-β cos α cos β sin α Let s use a unit circle
k A = [k, k]( )[a 1, a 2 ] = [ka 1,ka 2 ] 4For the division of two intervals of confidence in R +
Chapter 3. Fuzzy Arithmetic 3- Fuzzy arithmetic: ~Addition(+) and subtraction (-): Let A = [a and B = [b, b in R If x [a and y [b, b than x+y [a +b +b Symbolically,we write A(+)B = [a (+)[b, b = [a +b
Dr. D. Dinev, Department of Structural Mechanics, UACEG
Lecture 4 Material behavior: Constitutive equations Field of the game Print version Lecture on Theory of lasticity and Plasticity of Dr. D. Dinev, Department of Structural Mechanics, UACG 4.1 Contents
Strain gauge and rosettes
Strain gauge and rosettes Introduction A strain gauge is a device which is used to measure strain (deformation) on an object subjected to forces. Strain can be measured using various types of devices classified
Answers to practice exercises
Answers to practice exercises Chapter Exercise (Page 5). 9 kg 2. 479 mm. 66 4. 565 5. 225 6. 26 7. 07,70 8. 4 9. 487 0. 70872. $5, Exercise 2 (Page 6). (a) 468 (b) 868 2. (a) 827 (b) 458. (a) 86 kg (b)
1. Sketch the ground reactions on the diagram and write the following equations (in units of kips and feet). (8 points) ΣF x = 0 = ΣF y = 0 =
IDE S8 Test 6 Name:. Sketch the ground reactions on the diagram and write the following equations (in units of kips and feet). (8 points) ΣF x = = ΣF y = = ΣM A = = (counter-clockwise as positie). Sketch
MATHEMATICS. 1. If A and B are square matrices of order 3 such that A = -1, B =3, then 3AB = 1) -9 2) -27 3) -81 4) 81
1. If A and B are square matrices of order 3 such that A = -1, B =3, then 3AB = 1) -9 2) -27 3) -81 4) 81 We know that KA = A If A is n th Order 3AB =3 3 A. B = 27 1 3 = 81 3 2. If A= 2 1 0 0 2 1 then
ES440/ES911: CFD. Chapter 5. Solution of Linear Equation Systems
ES440/ES911: CFD Chapter 5. Solution of Linear Equation Systems Dr Yongmann M. Chung http://www.eng.warwick.ac.uk/staff/ymc/es440.html Y.M.Chung@warwick.ac.uk School of Engineering & Centre for Scientific
Inverse trigonometric functions & General Solution of Trigonometric Equations. ------------------ ----------------------------- -----------------
Inverse trigonometric functions & General Solution of Trigonometric Equations. 1. Sin ( ) = a) b) c) d) Ans b. Solution : Method 1. Ans a: 17 > 1 a) is rejected. w.k.t Sin ( sin ) = d is rejected. If sin
Trigonometry 1.TRIGONOMETRIC RATIOS
Trigonometry.TRIGONOMETRIC RATIOS. If a ray OP makes an angle with the positive direction of X-axis then y x i) Sin ii) cos r r iii) tan x y (x 0) iv) cot y x (y 0) y P v) sec x r (x 0) vi) cosec y r (y
ECE Spring Prof. David R. Jackson ECE Dept. Notes 2
ECE 634 Spring 6 Prof. David R. Jackson ECE Dept. Notes Fields in a Source-Free Region Example: Radiation from an aperture y PEC E t x Aperture Assume the following choice of vector potentials: A F = =
PARTIAL NOTES for 6.1 Trigonometric Identities
PARTIAL NOTES for 6.1 Trigonometric Identities tanθ = sinθ cosθ cotθ = cosθ sinθ BASIC IDENTITIES cscθ = 1 sinθ secθ = 1 cosθ cotθ = 1 tanθ PYTHAGOREAN IDENTITIES sin θ + cos θ =1 tan θ +1= sec θ 1 + cot
Rectangular Polar Parametric
Harold s Precalculus Rectangular Polar Parametric Cheat Sheet 15 October 2017 Point Line Rectangular Polar Parametric f(x) = y (x, y) (a, b) Slope-Intercept Form: y = mx + b Point-Slope Form: y y 0 = m
Problem 3.1 Vector A starts at point (1, 1, 3) and ends at point (2, 1,0). Find a unit vector in the direction of A. Solution: A = 1+9 = 3.
Problem 3.1 Vector A starts at point (1, 1, 3) and ends at point (, 1,0). Find a unit vector in the direction of A. Solution: A = ˆx( 1)+ŷ( 1 ( 1))+ẑ(0 ( 3)) = ˆx+ẑ3, A = 1+9 = 3.16, â = A A = ˆx+ẑ3 3.16
Exercises 10. Find a fundamental matrix of the given system of equations. Also find the fundamental matrix Φ(t) satisfying Φ(0) = I. 1.
Exercises 0 More exercises are available in Elementary Differential Equations. If you have a problem to solve any of them, feel free to come to office hour. Problem Find a fundamental matrix of the given
Lifting Entry (continued)
ifting Entry (continued) Basic planar dynamics of motion, again Yet another equilibrium glide Hypersonic phugoid motion Planar state equations MARYAN 1 01 avid. Akin - All rights reserved http://spacecraft.ssl.umd.edu
Second Order RLC Filters
ECEN 60 Circuits/Electronics Spring 007-0-07 P. Mathys Second Order RLC Filters RLC Lowpass Filter A passive RLC lowpass filter (LPF) circuit is shown in the following schematic. R L C v O (t) Using phasor
CHAPTER 12: PERIMETER, AREA, CIRCUMFERENCE, AND 12.1 INTRODUCTION TO GEOMETRIC 12.2 PERIMETER: SQUARES, RECTANGLES,
CHAPTER : PERIMETER, AREA, CIRCUMFERENCE, AND SIGNED FRACTIONS. INTRODUCTION TO GEOMETRIC MEASUREMENTS p. -3. PERIMETER: SQUARES, RECTANGLES, TRIANGLES p. 4-5.3 AREA: SQUARES, RECTANGLES, TRIANGLES p.
!! " &' ': " /.., c #$% & - & ' ()",..., * +,.. * ' + * - - * ()",...(.
..,.. 00 !!.6 7 " 57 +: #$% & - & ' ()",..., * +,.. * ' + * - - * ()",.....(. 8.. &' ': " /..,... :, 00. c. " *+ ' * ' * +' * - * «/'» ' - &, $%' * *& 300.65 «, + *'». 3000400- -00 3-00.6, 006 3 4.!"#"$
TeSys contactors a.c. coils for 3-pole contactors LC1-D
References a.c. coils for 3-pole contactors LC1-D Control circuit voltage Average resistance Inductance of Reference (1) Weight Uc at 0 C ± 10 % closed circuit For 3-pole " contactors LC1-D09...D38 and
Second Order Partial Differential Equations
Chapter 7 Second Order Partial Differential Equations 7.1 Introduction A second order linear PDE in two independent variables (x, y Ω can be written as A(x, y u x + B(x, y u xy + C(x, y u u u + D(x, y
2 Προετοιμαςία & χοριγθςθ IV υγρϊν. Όροι Χρήςησ
Προετοιμασία & χορήγηση IV υγρών 4θ Υγειιονομιικι Περιιφζρειια Μακεδονίίασ Θράκθσ 2 Προετοιμαςία & χοριγθςθ IV υγρϊν Όροι Χρήςησ Το πρωτόκολλο νοςθλευτικισ πρακτικισ, που ακολουκεί, αναπτφχκθκε από κλινικοφσ
is like multiplying by the conversion factor of. Dividing by 2π gives you the
Chapter Graphs of Trigonometric Functions Answer Ke. Radian Measure Answers. π. π. π. π. 7π. π 7. 70 8. 9. 0 0. 0. 00. 80. Multipling b π π is like multipling b the conversion factor of. Dividing b 0 gives
What happens when two or more waves overlap in a certain region of space at the same time?
Wave Superposition What happens when two or more waves overlap in a certain region of space at the same time? To find the resulting wave according to the principle of superposition we should sum the fields
Review Test 3. MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question.
Review Test MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. Find the exact value of the expression. 1) sin - 11π 1 1) + - + - - ) sin 11π 1 ) ( -
MECHANICAL PROPERTIES OF MATERIALS
MECHANICAL PROPERTIES OF MATERIALS! Simple Tension Test! The Stress-Strain Diagram! Stress-Strain Behavior of Ductile and Brittle Materials! Hooke s Law! Strain Energy! Poisson s Ratio! The Shear Stress-Strain
Delhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubaneswar Kolkata Patna Web: Ph:
Seria : 0. T_ME_(+B)_Strength of Materia_9078 Dehi Noida Bhopa Hyderabad Jaipur Luckno Indore une Bhubanesar Kokata atna Web: E-mai: info@madeeasy.in h: 0-56 CLSS TEST 08-9 MECHNICL ENGINEERING Subject
C 1 D 1. AB = a, AD = b, AA1 = c. a, b, c : (1) AC 1 ; : (1) AB + BC + CC1, AC 1 = BC = AD, CC1 = AA 1, AC 1 = a + b + c. (2) BD 1 = BD + DD 1,
1 1., BD 1 B 1 1 D 1, E F B 1 D 1. B = a, D = b, 1 = c. a, b, c : (1) 1 ; () BD 1 ; () F; D 1 F 1 (4) EF. : (1) B = D, D c b 1 E a B 1 1 = 1, B1 1 = B + B + 1, 1 = a + b + c. () BD 1 = BD + DD 1, BD =
θ p = deg ε n = με ε t = με γ nt = μrad
IDE 110 S08 Test 7 Name: 1. The strain components ε x = 946 με, ε y = -294 με and γ xy = -362 με are given for a point in a body subjected to plane strain. Determine the strain components ε n, ε t, and
Lecture 26: Circular domains
Introductory lecture notes on Partial Differential Equations - c Anthony Peirce. Not to be copied, used, or revised without eplicit written permission from the copyright owner. 1 Lecture 6: Circular domains
10/3/ revolution = 360 = 2 π radians = = x. 2π = x = 360 = : Measures of Angles and Rotations
//.: Measures of Angles and Rotations I. Vocabulary A A. Angle the union of two rays with a common endpoint B. BA and BC C. B is the vertex. B C D. You can think of BA as the rotation of (clockwise) with
Numerical Analysis FMN011
Numerical Analysis FMN011 Carmen Arévalo Lund University carmen@maths.lth.se Lecture 12 Periodic data A function g has period P if g(x + P ) = g(x) Model: Trigonometric polynomial of order M T M (x) =
1 String with massive end-points
1 String with massive end-points Πρόβλημα 5.11:Θεωρείστε μια χορδή μήκους, τάσης T, με δύο σημειακά σωματίδια στα άκρα της, το ένα μάζας m, και το άλλο μάζας m. α) Μελετώντας την κίνηση των άκρων βρείτε
Matrices and vectors. Matrix and vector. a 11 a 12 a 1n a 21 a 22 a 2n A = b 1 b 2. b m. R m n, b = = ( a ij. a m1 a m2 a mn. def
Matrices and vectors Matrix and vector a 11 a 12 a 1n a 21 a 22 a 2n A = a m1 a m2 a mn def = ( a ij ) R m n, b = b 1 b 2 b m Rm Matrix and vectors in linear equations: example E 1 : x 1 + x 2 + 3x 4 =
2 Διενζργεια Διενζργεια υψθλοφ εκκενωτικοφ υποκλυςμοφ. Όροι Χρήςησ
Διενϋργεια Υψηλού Εκκενωτικού Υποκλυςμού 4η Υγειιονομιικό Περιιφϋρειια Μακεδονύύασ Θρϊκησ 2 Διενζργεια Διενζργεια υψθλοφ εκκενωτικοφ υποκλυςμοφ Όροι Χρήςησ Το πρωτόκολλο νοςθλευτικισ πρακτικισ, που ακολουκεί,
University of Waterloo. ME Mechanical Design 1. Partial notes Part 1
University of Waterloo Department of Mechanical Engineering ME 3 - Mechanical Design 1 Partial notes Part 1 G. Glinka Fall 005 1 Forces and stresses Stresses and Stress Tensor Two basic types of forces
SCHOOL OF MATHEMATICAL SCIENCES G11LMA Linear Mathematics Examination Solutions
SCHOOL OF MATHEMATICAL SCIENCES GLMA Linear Mathematics 00- Examination Solutions. (a) i. ( + 5i)( i) = (6 + 5) + (5 )i = + i. Real part is, imaginary part is. (b) ii. + 5i i ( + 5i)( + i) = ( i)( + i)
Theoretical Question 2: Strong Resistive Electromagnets SOLUTION
25 April 2 Page of 6 (Document Released: 4:3, 4/24) Theoretical Question 2: Strong Resistive Electromagnets SOLUTION Part A. Magnetic Fields on the Axis of the Coil (a) At the point xx on the axis, the
( ) 2 and compare to M.
Problems and Solutions for Section 4.2 4.9 through 4.33) 4.9 Calculate the square root of the matrix 3!0 M!0 8 Hint: Let M / 2 a!b ; calculate M / 2!b c ) 2 and compare to M. Solution: Given: 3!0 M!0 8
ANSWERSHEET (TOPIC = DIFFERENTIAL CALCULUS) COLLECTION #2. h 0 h h 0 h h 0 ( ) g k = g 0 + g 1 + g g 2009 =?
Teko Classes IITJEE/AIEEE Maths by SUHAAG SIR, Bhopal, Ph (0755) 3 00 000 www.tekoclasses.com ANSWERSHEET (TOPIC DIFFERENTIAL CALCULUS) COLLECTION # Question Type A.Single Correct Type Q. (A) Sol least
SIEMENS Squirrel Cage Induction Standard Three-phase Motors
- SIEMENS Squirrel Cage Induction Standard Three-phase Motors 2 pole 3000 rpm 50Hz Rated current Power Efficiency Rated Ratio Noise Output Frame Speed Weight 3V 400V 415V factor Class 0%Load 75%Load torque
Mechanics of Materials Lab
Mechanics of Materials Lab Lecture 9 Strain and lasticity Textbook: Mechanical Behavior of Materials Sec. 6.6, 5.3, 5.4 Jiangyu Li Jiangyu Li, Prof. M.. Tuttle Strain: Fundamental Definitions "Strain"
Lifting Entry 2. Basic planar dynamics of motion, again Yet another equilibrium glide Hypersonic phugoid motion MARYLAND U N I V E R S I T Y O F
ifting Entry Basic planar dynamics of motion, again Yet another equilibrium glide Hypersonic phugoid motion MARYAN 1 010 avid. Akin - All rights reserved http://spacecraft.ssl.umd.edu ifting Atmospheric
UNIVERSITY OF CAMBRIDGE INTERNATIONAL EXAMINATIONS General Certificate of Education Ordinary Level
UNIVERSITY OF CAMBRIDGE INTERNATIONAL EXAMINATIONS General Certificate of Education Ordinary Level * 6 3 1 7 7 7 6 4 0 6 * MATHEMATICS (SYLLABUS D) 4024/21 Paper 2 October/November 2013 Candidates answer
1. In calculating the shear flow associated with the nail shown, which areas should be included in the calculation of Q? (3 points) Areas (1) and (5)
IDE 0 S08 Test 5 Name:. In calculating the shear flow associated with the nail shown, which areas should be included in the calculation of Q? ( points) Areas () and (5) Areas () through (5) Areas (), ()
Chapter 2. Stress, Principal Stresses, Strain Energy
Chapter Stress, Principal Stresses, Strain nergy Traction vector, stress tensor z z σz τ zy ΔA ΔF A ΔA ΔF x ΔF z ΔF y y τ zx τ xz τxy σx τ yx τ yz σy y A x x F i j k is the traction force acting on the
CHAPTER 48 APPLICATIONS OF MATRICES AND DETERMINANTS
CHAPTER 48 APPLICATIONS OF MATRICES AND DETERMINANTS EXERCISE 01 Page 545 1. Use matrices to solve: 3x + 4y x + 5y + 7 3x + 4y x + 5y 7 Hence, 3 4 x 0 5 y 7 The inverse of 3 4 5 is: 1 5 4 1 5 4 15 8 3
Derivations of Useful Trigonometric Identities
Derivations of Useful Trigonometric Identities Pythagorean Identity This is a basic and very useful relationship which comes directly from the definition of the trigonometric ratios of sine and cosine
Lecture 2: Dirac notation and a review of linear algebra Read Sakurai chapter 1, Baym chatper 3
Lecture 2: Dirac notation and a review of linear algebra Read Sakurai chapter 1, Baym chatper 3 1 State vector space and the dual space Space of wavefunctions The space of wavefunctions is the set of all
Spherical Coordinates
Spherical Coordinates MATH 311, Calculus III J. Robert Buchanan Department of Mathematics Fall 2011 Spherical Coordinates Another means of locating points in three-dimensional space is known as the spherical
Περίπτωση Μελέτης Θαλάσσιας Κατασκευής με χρήση λογισμικού και με βάση Κώδικες (Compliant Tower) (8.1.10)
Επιχειρησιακό Πρόγραμμα Εκπαίδευση και ια Βίου Μάθηση Πρόγραμμα ια Βίου Μάθησης ΑΕΙ για την Επικαιροποίηση Γνώσεων Αποφοίτων ΑΕΙ: Σύγχρονες Εξελίξεις στις Θαλάσσιες Κατασκευές Α.Π.Θ. Πολυτεχνείο Κρήτης
Supplementary Information 1.
Supplementary Information 1. Fig. S1. Correlations between litter-derived-c and N (percent of initial input) and Al-/Fe- (hydr)oxides dissolved by ammonium oxalate (AO); a) 0 10 cm; b) 10 20 cm; c) 20
Jordan Form of a Square Matrix
Jordan Form of a Square Matrix Josh Engwer Texas Tech University josh.engwer@ttu.edu June 3 KEY CONCEPTS & DEFINITIONS: R Set of all real numbers C Set of all complex numbers = {a + bi : a b R and i =
DETERMINATION OF DYNAMIC CHARACTERISTICS OF A 2DOF SYSTEM. by Zoran VARGA, Ms.C.E.
DETERMINATION OF DYNAMIC CHARACTERISTICS OF A 2DOF SYSTEM by Zoran VARGA, Ms.C.E. Euro-Apex B.V. 1990-2012 All Rights Reserved. The 2 DOF System Symbols m 1 =3m [kg] m 2 =8m m=10 [kg] l=2 [m] E=210000
Pg The perimeter is P = 3x The area of a triangle is. where b is the base, h is the height. In our case b = x, then the area is
Pg. 9. The perimeter is P = The area of a triangle is A = bh where b is the base, h is the height 0 h= btan 60 = b = b In our case b =, then the area is A = = 0. By Pythagorean theorem a + a = d a a =
9.09. # 1. Area inside the oval limaçon r = cos θ. To graph, start with θ = 0 so r = 6. Compute dr
9.9 #. Area inside the oval limaçon r = + cos. To graph, start with = so r =. Compute d = sin. Interesting points are where d vanishes, or at =,,, etc. For these values of we compute r:,,, and the values
Matrices Review. Here is an example of matrices multiplication for a 3x3 matrix
Matrices Review Matri Multiplication : When the number of columns of the first matri is the same as the number of rows in the second matri then matri multiplication can be performed. Here is an eample
Answers - Worksheet A ALGEBRA PMT. 1 a = 7 b = 11 c = 1 3. e = 0.1 f = 0.3 g = 2 h = 10 i = 3 j = d = k = 3 1. = 1 or 0.5 l =
C ALGEBRA Answers - Worksheet A a 7 b c d e 0. f 0. g h 0 i j k 6 8 or 0. l or 8 a 7 b 0 c 7 d 6 e f g 6 h 8 8 i 6 j k 6 l a 9 b c d 9 7 e 00 0 f 8 9 a b 7 7 c 6 d 9 e 6 6 f 6 8 g 9 h 0 0 i j 6 7 7 k 9
ο αεροσολσ σλοω χλιµατιχ ωαρµινγ? Ηαλτινγ τηε σπρεαδ οφ ΑΙ Σ. Χαν παρτιχλε πηψσιχσ χοµε βαχκ?
ΦΕΒΡΥΑΡΨ 1994 3.95 ο αεροσολσ σλοω χλιµατιχ ωαρµινγ? Ηαλτινγ τηε σπρεαδ οφ ΑΙ Σ. Χαν παρτιχλε πηψσιχσ χοµε βαχκ? ιγιταλ φοργερψ χαν χρεατε πηοτογραπηιχ εϖιδενχε φορ εϖεντσ τηατ νεϖερ ηαππενεδ. Φεβρυαρψ
Homework 3 Solutions
Homework 3 Solutions Igor Yanovsky (Math 151A TA) Problem 1: Compute the absolute error and relative error in approximations of p by p. (Use calculator!) a) p π, p 22/7; b) p π, p 3.141. Solution: For
Practice Exam 2. Conceptual Questions. 1. State a Basic identity and then verify it. (a) Identity: Solution: One identity is csc(θ) = 1
Conceptual Questions. State a Basic identity and then verify it. a) Identity: Solution: One identity is cscθ) = sinθ) Practice Exam b) Verification: Solution: Given the point of intersection x, y) of the
b. Use the parametrization from (a) to compute the area of S a as S a ds. Be sure to substitute for ds!
MTH U341 urface Integrals, tokes theorem, the divergence theorem To be turned in Wed., Dec. 1. 1. Let be the sphere of radius a, x 2 + y 2 + z 2 a 2. a. Use spherical coordinates (with ρ a) to parametrize.
!"#$%& '!(#)& a<.21c67.<9 /06 :6>/ 54.6: 1. ]1;A76 _F -. /06 4D26.36 <> A.:4D6:6C C4/4 /06 D:43? C</ O=47?6C b*dp 12 :1?6:E /< D6 3:4221N6C 42 D:A6 O=
! " #$% & '( )*+, -. /012 3045/67 8 96 57626./ 4. 4:;74= 69676.36 D426C
DuPont Suva 95 Refrigerant
Technical Information T-95 ENG DuPont Suva refrigerants Thermodynamic Properties of DuPont Suva 95 Refrigerant (R-508B) The DuPont Oval Logo, The miracles of science, and Suva, are trademarks or registered
Ingenieurbüro Frank Blasek - Beratender Ingenieur Am Kohlhof 10, Osterholz-Scharmbeck Tel: 04791/ Fax: 04791/
Page: 10 CONTENTS Contents... 10 General Data... 10 Structural Data des... 10 erials... 10 Sections... 10 ents... 11 Supports... 11 Loads General Data... 12 LC 1 - Vollast 120 km/h 0,694 kn/qm... 12 LC,
Ingenieurbüro Frank Blasek - Beratender Ingenieur Am Kohlhof 10, Osterholz-Scharmbeck Tel: 04791/ Fax: 04791/
Page: 1 CONTENTS Contents... 1 General Data... 1 Structural Data des... 1 erials... 1 Sections... 1 ents... 2 Supports... 2 Loads General Data... 3 LC 1 - Vollast 90 km/h 0,39 kn/qm... 3 LC, LG Results
UNIVERSITY OF CAMBRIDGE INTERNATIONAL EXAMINATIONS General Certificate of Education Ordinary Level
UNIVERSITY OF CAMBRIDGE INTERNATIONAL EXAMINATIONS General Certificate of Education Ordinary Level * 0 5 1 0 3 4 8 7 8 5 * MATHEMATICS (SYLLABUS D) 4024/21 Paper 2 May/June 2013 Candidates answer on the
DuPont Suva. DuPont. Thermodynamic Properties of. Refrigerant (R-410A) Technical Information. refrigerants T-410A ENG
Technical Information T-410A ENG DuPont Suva refrigerants Thermodynamic Properties of DuPont Suva 410A Refrigerant (R-410A) The DuPont Oval Logo, The miracles of science, and Suva, are trademarks or registered
Chapter 7 Analytic Trigonometry
Chapter 7 Analytic Trigonometry Section 7.. Domain: { is any real number} ; Range: { y y }. { } or { }. [, ). True. ;. ; 7. sin y 8. 0 9. 0. False. The domain of. True. True.. y sin is. sin 0 We are finding
KEPKYPA Â Î Û Â È KEPKYPA
KEPKYPA Â Î Û Â È KEPKYPA ISBN: 978-960-9490-06-1 Copyright: Εκδόσεις ΚΕΡΚΥΡΑ Α.Ε. Economia PUBLISHING 1η έκδοση, Νοέµβριος 2010 Ελεύθερη έµµετρη απόδοση: ηµήτρης Β. Χρυσοβιτσιώτης Εικονογράφηση: Ειρήνη
1. (a) (5 points) Find the unit tangent and unit normal vectors T and N to the curve. r(t) = 3cost, 4t, 3sint
1. a) 5 points) Find the unit tangent and unit normal vectors T and N to the curve at the point P, π, rt) cost, t, sint ). b) 5 points) Find curvature of the curve at the point P. Solution: a) r t) sint,,
CHAPTER (2) Electric Charges, Electric Charge Densities and Electric Field Intensity
CHAPTE () Electric Chrges, Electric Chrge Densities nd Electric Field Intensity Chrge Configurtion ) Point Chrge: The concept of the point chrge is used when the dimensions of n electric chrge distriution
Chapter 6 BLM Answers
Chapter 6 BLM Answers BLM 6 Chapter 6 Prerequisite Skills. a) i) II ii) IV iii) III i) 5 ii) 7 iii) 7. a) 0, c) 88.,.6, 59.6 d). a) 5 + 60 n; 7 + n, c). rad + n rad; 7 9,. a) 5 6 c) 69. d) 0.88 5. a) negative
The Simply Typed Lambda Calculus
Type Inference Instead of writing type annotations, can we use an algorithm to infer what the type annotations should be? That depends on the type system. For simple type systems the answer is yes, and
Differentiation exercise show differential equation
Differentiation exercise show differential equation 1. If y x sin 2x, prove that x d2 y 2 2 + 2y x + 4xy 0 y x sin 2x sin 2x + 2x cos 2x 2 2cos 2x + (2 cos 2x 4x sin 2x) x d2 y 2 2 + 2y x + 4xy (2x cos
26 28 Find an equation of the tangent line to the curve at the given point Discuss the curve under the guidelines of Section
SECTION 5. THE NATURAL LOGARITHMIC FUNCTION 5. THE NATURAL LOGARITHMIC FUNCTION A Click here for answers. S Click here for solutions. 4 Use the Laws of Logarithms to epand the quantit.. ln ab. ln c. ln
The logic of the Mechanics of Materials
Torsion The logic of the Mechanics of Materials Torsion Chapter 5 Torsion Torsional failures (ductile, buckling, buckling): Bars subjected to Torsion Let us now consider a straight bar supported at one
Written Examination. Antennas and Propagation (AA ) April 26, 2017.
Written Examination Antennas and Propagation (AA. 6-7) April 6, 7. Problem ( points) Let us consider a wire antenna as in Fig. characterized by a z-oriented linear filamentary current I(z) = I cos(kz)ẑ
5.0 DESIGN CALCULATIONS
5.0 DESIGN CALCULATIONS Load Data Reference Drawing No. 2-87-010-80926 Foundation loading for steel chimney 1-00-281-53214 Boiler foundation plan sketch : Figure 1 Quantity Unit Dia of Stack, d 6.00 m