a. Radiation, ultrasonic, brittle and ductile
b. Concentrated, simple, uniform and random
c. Tense, counteractive, reactive, centrifugal and opposite
d. Torsional, compressive, uniform, shear and tensile
e. Torsional, compressive, bending, shear and tensile
d. Torsional, compressive, uniform, shear and tensile
a. Bending
b. Shearing
c. Torsional
d. Compressive
e. Tensile
b. Shearing
a. Strain
b. Stress
c. Set
d. Variable
e. Elastic limit
a. Strain
a. Linear stress
b. Compressive stress
c. Axial stress
d. Linear strain
e. Axial thrust
d. Linear strain
a. The compressive stress
b. Tensile stress
c. Linear strain
d. Tensile strain
e. Shearing strain
c. Linear strain
a. Shearing
b. Double shear
c. Torsional
d. Bending
e. Tensile
e. Tensile
a. Deformation per unit length
b. Force which causes a change in body shape
c. Original length multiplied by the change in length
d. Original length divided by the change in length
e. Original length divided by the change in area
a. Deformation per unit length
a. Toughness
b. Hardness
c. Plasticity
d. Elastic properties
e. Ductility
d. Elastic properties
a. The yield point of the material is exceeded
b. The elastic limits of the material is not exceeded
c. The elastic limits of the material is exceeded
d. Young’s Modulus remains constant
e. The yield point of the material is not exceeded
b. The elastic limits of the material is not exceeded
a. Area to load on a body
b. Change in length to original length of a body
c. Stress to strain relation of a body
d. Unit stress of a body
e. Unit strain of a body
c. Stress to strain relation of a body
a. The deformation produced is directly proportional to the stress producing it.
b. The strain produced is indirectly proportional to the stress producing it.
c. The strain produced is inversely proportional to the stress producing it.
d. The deformation produced is directly proportional to the strain producing it.
e. The deformation produced is inversely proportional to the stress producing it.
a. The deformation produced is directly proportional to the stress producing it.
a. The sum of increment of stress to increment of strain
b. The grain alignment within a body.
c. The average of increments of stress to increment of strain.
d. The product of increment of stress to increment of strain.
e. The ratio of increment of stress to increment of strain.
e. The ratio of increment of stress to increment of strain.
a. Elastic limit of a specimen.
b. Young’s Modulus where E = stress divided by strain.
c. Elastic section modulus where E = area divided by strain.
d. Young’s Modulus where E = strain divided by stress.
e. Young’s Modulus where E = strain multiplied by stress.
b. Young’s Modulus where E = stress divided by strain.
a. Area of the body
b. Bending moments
c. Amount of strain produced
d. Moment of force
e. The original length
c. Amount of strain produced
a. Shows no sign of strain due to loading when the load is removed
b. Maintains a new length or shape after the load is removed
c. Can only be loaded to the yield point
d. Will take any shape due to elastic ability
e. Can only be loaded to the elastic limit
a. Shows no sign of strain due to loading when the load is removed
a. Joules
b. kPa
c. Newtons per second
d. Newtons per hour
e. kN
b. kPa
a. Young’s Modulus
b. Hooke’s Law
c. Modulus of elasticity
d. None of the above
b. Hooke’s Law
a. Less than the allowable working stress
b. Greater than the allowable working stress
c. Equal to the allowable working stress
d. Varied as to greater or less than the allowable working stress depending upon the load applied
e. Ten times greater than the allowable stress
b. Greater than the allowable working stress
a. The elastic limit
b. The load at which the sample breaks
c. The yield point
d. When the maximum elongation is obtained without rupture to the sample
e. Before the yield point
b. The load at which the sample breaks
a. Kilowatts
b. Square metres
c. Kilopascals
d. Joules
e. Kilo Newtons
c. Kilopascals
a. That area at the point when the elastic limit is reached
b. That area when the maximum load is applied
c. That area when the yield point is reached
d. That area known prior to the test
e. That area before the elastic limit is reached
b. That area when the maximum load is applied
a. Subtracting the safe working stress from the ultimate strength
b. Dividing the ultimate strength by the safe working stress
c. Dividing the safe working stress by the ultimate strength
d. Dividing the difference between the safe working stress and the ultimate strength into the ultimate strength
e. Multiplying the ultimate strength by the safe working stress
b. Dividing the ultimate strength by the safe working stress
a. Brittleness
b. Ductility
c. Ultimate strength
d. Stiffness
e. Hardness
c. Ultimate strength
a. True
b. False
b. False