Strength of Materials Practice Flashcards

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100 flashcards covering Strength of Materials concepts from the lecture transcript, including material properties, stresses, beams, torsion, and columns.

Last updated 5:41 PM on 8/7/26
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102 Terms

1
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What is a Homogeneous Material?

A material which have same elastic properties at any point in a given direction.

2
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What is an Isotropic Material?

This material has same identical properties in all direction at a point.

3
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What is an Anisotropic Material?

It has different properties in all direction at a point in the body.

4
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What is an Orthotropic Material?

A material which has different properties in three mutually perpendicular planes.

5
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What is the Poisson's Ratio for Cork?

00

6
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What is the Poisson's Ratio range for Glass?

0.020.030.02 - 0.03

7
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What is the Poisson's Ratio range for Cast Iron?

0.230.270.23 - 0.27

8
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What is the Poisson's Ratio range for Elastic Material?

0.250.400.25 - 0.40

9
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What is the Poisson's Ratio range for Steel?

0.270.330.27 - 0.33

10
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What is the Poisson's Ratio for Rubber?

0.500.50

11
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What is the Poisson's Ratio for Human Tissues?

1-1

12
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What is the Poisson's Ratio for Wrought Iron?

0.300.30

13
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What is the Poisson's Ratio range for Concrete?

0.100.200.10 - 0.20

14
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What is the formula for Young's Modulus (E)?

E=Longitudinal StressLongitudinal Strain=σϵE = \frac{\text{Longitudinal Stress}}{\text{Longitudinal Strain}} = \frac{\sigma}{\epsilon}

15
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How is Modulus of Rigidity or Shear Modulus (G) defined?

G=Shear stressShear strain=τϕG = \frac{\text{Shear stress}}{\text{Shear strain}} = \frac{\tau}{\phi}

16
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What is the formula for Poisson's Ratio (\mu)?

μ=Lateral StrainLinear Strain=δd/dδl/l\mu = -\frac{\text{Lateral Strain}}{\text{Linear Strain}} = -\frac{\delta d / d}{\delta l / l}

17
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What is the formula for Bulk Modulus (K)?

K=Direct stressVolumetric Strain=σϵvK = \frac{\text{Direct stress}}{\text{Volumetric Strain}} = \frac{\sigma}{\epsilon_v}

18
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What is the stress formula for a Gradual load?

σ=PA\sigma = \frac{P}{A}

19
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How is stress calculated for a Sudden load?

σsudden=2×PA\sigma_{\text{sudden}} = 2 \times \frac{P}{A}

20
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What is the stress formula for an Impact load?

σi=WA(1+1+2hAEWl)\sigma_i = \frac{W}{A} \left( 1 + \sqrt{1 + \frac{2hAE}{Wl}} \right)

21
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What is the relation between E, G, and \mu?

E=2G(1+μ)E = 2G (1+\mu)

22
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What is the relation between E, K, and \mu?

E=3K(12μ)E = 3K(1-2\mu)

23
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What is the formula for E in terms of K and G?

E=9KG3K+GE = \frac{9KG}{3K + G}

24
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What is the formula for \mu in terms of K and G?

μ=3K2G6K+2G\mu = \frac{3K - 2G}{6K + 2G}

25
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How many independent elastic constants are there for Homogeneous and Isotropic materials?

22

26
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How many total number of elastic constants are there for Homogeneous and Isotropic materials?

44

27
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How many independent elastic constants are there for Orthotropic materials (like wood)?

99

28
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How many total number of elastic constants are there for Orthotropic materials?

1212

29
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How many independent elastic constants are there for Anisotropic materials?

2121

30
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How many total number of elastic constants are there for Anisotropic materials?

\infty

31
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What is the axial elongation formula for a Prismatic bar due to external load?

δl=PlAE\delta l = \frac{Pl}{AE}

32
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What is the elongation formula for a Circular tapered bar?

δl=4Plπd1d2E\delta l = \frac{4Pl}{\pi d_1 d_2 E}

33
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What is the elongation formula for a Rectangular tapered bar?

δl=Pl(b2b1)Etln(b2b1)\delta l = \frac{Pl}{(b_2 - b_1)Et} \ln \left( \frac{b_2}{b_1} \right)

34
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In Composite bars, what is the relateion between total load P and segment loads?

P=P1+P2P = P_1 + P_2

35
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What is the elongation of a Prismatic bar due to self weight?

δl=ρgl22E=wl22E\delta l = \frac{\rho g l^2}{2E} = \frac{wl^2}{2E}

36
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What is the elongation of a Uniform tapering or conical bar due to self weight?

δc=γl26E=Wl2AE×13\delta_c = \frac{\gamma l^2}{6E} = \frac{Wl}{2AE} \times \frac{1}{3}

37
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What is the relationship between the elongation of a conical bar and a prismatic bar of same length and load?

δc=13δP\delta_c = \frac{1}{3} \delta_P

38
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What is the thermal stress in Case 1 (Free expansion or contraction)?

σth=0\sigma_{\text{th}} = 0

39
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What is the thermal stress in Case 2 (Fully prevented)?

σth=EαΔT\sigma_{\text{th}} = E\alpha \Delta T

40
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What is the thermal stress formula for Case 3 (Partially prevented by distance x)?

σth=El(lαΔTx)\sigma_{\text{th}} = \frac{E}{l} (l\alpha \Delta T - x)

41
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What is the thermal stress formula for a Taper section?

σth=d2d1EαΔT\sigma_{\text{th}} = \frac{d_2}{d_1} E \alpha \Delta T

42
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What is the formula for True stress (σT\sigma_T)?

σT=PAi\sigma_T = \frac{P}{A_i}

43
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What is the formula for True strain (ϵT\epsilon_T)?

ϵT=ln(lilo)\epsilon_T = \ln \left( \frac{l_i}{l_o} \right)

44
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What is the relationship between True stress and Engineering stress (σe\sigma_e)?

σT=σe(1+e)\sigma_T = \sigma_e ( 1 + e )

45
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What is the relationship between True strain and Engineering strain (e)?

ϵT=ln(1+e)\epsilon_T = \ln ( 1 + e )

46
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What is the Young's Modulus (E) of Steel?

2×105MPa2 \times 10^5 \, \text{MPa}

47
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What is the Young's Modulus (E) of Copper?

1.17×105MPa1.17 \times 10^5 \, \text{MPa}

48
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What is the Young's Modulus (E) of Aluminium?

0.70×105MPa0.70 \times 10^5 \, \text{MPa}

49
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What is the definition of Proof resilience?

Energy absorbed by body upto elastic limit.

50
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What is the formula for Modulus of resilience?

U=σmax22EU = \frac{\sigma_{max}^2}{2E}

51
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Which theory of failure was given by Rankine and is suitable for Brittle materials?

Maximum Principal Stress or normal stress theory.

52
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Which theory of failure was given by St. Venants?

Maximum Principal Strain theory.

53
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Guest & Trasca's theory is suitable for which type of material?

Ductile

54
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What is the graphical representation for the Maximum Principal Strain theory?

Rhombus

55
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Which theory of failure is associated with Vonmises and Hencky?

Maximum Shear Strain Energy theory.

56
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What is the formula for Normal stress (σn\sigma_n) on any plane?

σn=σx+σy2+σxσy2cos(2θ)+τxysin(2θ)\sigma_n = \frac{\sigma_x + \sigma_y}{2} + \frac{\sigma_x - \sigma_y}{2} \cos(2\theta) + \tau_{xy} \sin(2\theta)

57
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What is the formula for Tangential or shear stress (\tau) on any plane?

τ=σxσy2sin(2θ)+τxycos(2θ)\tau = -\frac{\sigma_x - \sigma_y}{2} \sin(2\theta) + \tau_{xy} \cos(2\theta)

58
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What is the formula to find the Principal Plane (θ\theta)?

tan(2θ)=2τxyσxσy\tan(2\theta) = \frac{2\tau_{xy}}{\sigma_x - \sigma_y}

59
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In Case-1 (Uniaxial load), what is the formula for Shear stress (\tau)?

τ=P2Asin(2α)\tau = \frac{P}{2A} \sin(2\alpha)

60
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How is the Radius of Mohr's circle (\tau_{max}) calculated?

R=σ1σ22=(σxσy2)2+τxy2R = \frac{\sigma_1 - \sigma_2}{2} = \sqrt{ \left( \frac{\sigma_x - \sigma_y}{2} \right)^2 + \tau_{xy}^2 }

61
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What is the coordinates for the Center of Mohr's circle?

(σx+σy2,0)\left( \frac{\sigma_x + \sigma_y}{2}, 0 \right)

62
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What does the rate of change of shear force (dV/dxdV/dx) equal?

W-W (load)

63
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What does the rate of change of bending moment (dM/dxdM/dx) equal?

VV (shear force)

64
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State the governing Bending equation for a beam.

MI=σby=ER\frac{M}{I} = \frac{\sigma_b}{y} = \frac{E}{R}

65
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What is the definition of Section modulus (Z)?

Z=IyZ = \frac{I}{y}

66
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What is the formula for Flexural Rigidity?

E×IE \times I

67
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What is the Moment of Inertia (IXXI_{XX}) for a Rectangular section?

bd312\frac{bd^3}{12}

68
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What is the Section Modulus (Z) for a Rectangular section?

bd26\frac{bd^2}{6}

69
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What is the Moment of Inertia (IbaseI_{base}) for a Triangular section?

bh312\frac{bh^3}{12}

70
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What is the Section Modulus (Z) for a Solid Circular section?

πD332\frac{\pi D^3}{32}

71
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What is the Moment of Inertia (IXXI_{XX}) for a Solid Circular section?

πD464\frac{\pi D^4}{64}

72
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What is the Moment of Inertia (IXXI_{XX}) for a Square section?

a412\frac{a^4}{12}

73
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What is the ratio of τmax\tau_{max} to τavg\tau_{avg} for a rectangular section?

32\frac{3}{2}

74
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What is the ratio of τmax\tau_{max} to τavg\tau_{avg} for a circular section?

43\frac{4}{3}

75
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State the Pure Torsion equation.

TJ=τR=GθL\frac{T}{J} = \frac{\tau}{R} = \frac{G\theta}{L}

76
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What is the formula for Shear stress (\tau) in a shaft subjected to torque T?

τ=16TπD3\tau = \frac{16T}{\pi D^3}

77
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What is the formula for Power (P) transmitted by a shaft in kW?

P = \frac{2\n̐ NT}{60 \times 1000}

78
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What is the formula for Polar section modulus (ZPZ_P)?

Zp=JRZ_p = \frac{J}{R}

79
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What is the Polar Moment of Inertia (J) for a solid shaft?

πd432\frac{\pi d^4}{32}

80
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What are the conditions for shafts connected in Parallel?

T=T1+T2T = T_1 + T_2 and θ1=θ2\theta_1 = \theta_2

81
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What are the conditions for shafts connected in Series?

T1=T2=TT_1 = T_2 = T and θ=θ1+θ2\theta = \theta_1 + \theta_2

82
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According to maximum shear stress theory, what is the maximum shear stress (τmax\tau_{max}) for combined loading?

τmax=12σb2+4τ2\tau_{max} = \frac{1}{2} \sqrt{\sigma_b^2 + 4\tau^2}

83
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What is the Equivalent Torque (TeT_e) formula?

Te=M2+T2T_e = \sqrt{M^2 + T^2}

84
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What is the Equivalent Bending Moment (MeM_e) formula?

Me=12(M+M2+T2)M_e = \frac{1}{2} \left( M + \sqrt{M^2 + T^2} \right)

85
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Name one method used to determine Slope and Deflection.

Macaulay's Method (or Double Integration, Area Moment, Strain energy, Conjugate Beam, Superposition).

86
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What is the maximum deflection (ymaxy_{max}) for a cantilever beam with a point load W at the free end?

WL33EI\frac{WL^3}{3EI}

87
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What is the maximum slope (θmax\theta_{max}) for a cantilever beam with a point load W at the free end?

WL22EI\frac{WL^2}{2EI}

88
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What is the maximum deflection (ymaxy_{max}) for a cantilever beam with UDL (w) over the entire length?

wL48EI\frac{wL^4}{8EI}

89
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What is the maximum deflection (ymaxy_{max}) for a simply supported beam with a central point load W?

WL348EI\frac{WL^3}{48EI}

90
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What is the maximum deflection (ymaxy_{max}) for a simply supported beam with UDL (w)?

5wL4384EI\frac{5wL^4}{384EI}

91
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What is the formula for Strain energy (U) due to axial loading on a uniform bar?

U=P2L2AEU = \frac{P^2 L}{2AE}

92
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What is the formula for Hoop stress (σH\sigma_H) in a thin cylinder?

σH=PD2t\sigma_H = \frac{PD}{2t}

93
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What is the formula for Longitudinal stress (σL\sigma_L) in a thin cylinder?

σL=PD4t\sigma_L = \frac{PD}{4t}

94
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What is the relation between Hoop stress and Longitudinal stress in a thin cylinder?

\sigma_h = 2 ̐ \sigma_L

95
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What is the formula for Volumetric strain (\epsilon_v) in a thin sphere?

ϵv=3PD4tE(1μ)\epsilon_v = \frac{3PD}{4tE} (1 - \mu)

96
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How is the Slenderness ratio (S.R.) defined?

S.R.=leKminS.R. = \frac{l_e}{K_{min}} (Effective length / Minimum radius of gyration).

97
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What is the failure mode for a Long column (S.R. > 120)?

Buckling

98
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What is the Euler's critical load (PcrP_{cr}) formula?

Pcr=π2EIminle2P_{cr} = \frac{\pi^2 EI_{min}}{l_e^2}

99
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What is the effective length (lel_e) for a column with one end fixed and other end free?

le=2Ll_e = 2L

100
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What is the effective length (lel_e) for a column with both ends hinged?

le=Ll_e = L