MCQOPTIONS
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MCQOPTIONS
This section includes 1232 Mcqs, each offering curated multiple-choice questions to sharpen your Electrical Engineering knowledge and support exam preparation. Choose a topic below to get started.
| 651. |
mild steel, gold, silver, copper, aluminium, etc. shows type of fracture |
| A. | cleavege |
| B. | cupcone |
| C. | star |
| D. | irregular fibrous |
| Answer» C. star | |
| 652. |
cast iron, glass, concrete, bricks etc. shows                type of fracture |
| A. | cleavege |
| B. | cupcone |
| C. | star |
| D. | irregular fibrous |
| Answer» B. cupcone | |
| 653. |
during tensile test, type of loading should be avoided |
| A. | shear |
| B. | eccentric |
| C. | repetitive |
| D. | all of the above |
| Answer» E. | |
| 654. |
               states that geometrically similar samples having constant L/D ratio shows same % elongation |
| A. | hooke\s law |
| B. | barba\s law |
| C. | newton\s law |
| D. | none of the above |
| Answer» C. newton\s law | |
| 655. |
during tensile test, if gauge length                  percentage elongation increases due to localised elongation |
| A. | decreases |
| B. | increases |
| C. | same |
| D. | all of the above |
| Answer» B. increases | |
| 656. |
in tensile test, during strain hardening material after cold working shows                      in strength with decreased toughness |
| A. | decrease |
| B. | increase |
| C. | no change |
| D. | none of the above |
| Answer» C. no change | |
| 657. |
for brittle material its |
| A. | yield stress and uts are very close |
| B. | uts and breaking are very close |
| C. | yield stress and uts and breaking are very close |
| D. | none of the above |
| Answer» D. none of the above | |
| 658. |
unit of toughness is |
| A. | pascal |
| B. | joule |
| C. | newton |
| D. | watts |
| Answer» C. newton | |
| 659. |
                     is the minimum value of stress in plastic region |
| A. | uts |
| B. | proof stress |
| C. | yield stress |
| D. | breaking stress |
| Answer» E. | |
| 660. |
for ducttile material is the maximum value of stress the material can sustain |
| A. | uts |
| B. | proof stress |
| C. | yield stress |
| D. | proportional stress |
| Answer» B. proof stress | |
| 661. |
Breaking Stress is also called as |
| A. | proof stress |
| B. | yield stress |
| C. | fracture stress |
| D. | uts |
| Answer» D. uts | |
| 662. |
             is the maximum value of stress in the plastic region |
| A. | uts |
| B. | proof stress |
| C. | yield stress |
| D. | proportional stress |
| Answer» B. proof stress | |
| 663. |
to calclulate proof stress, method is used |
| A. | offset |
| B. | bending |
| C. | shear |
| D. | all of the above |
| Answer» B. bending | |
| 664. |
                 is maximum value of stress upto which stress is directly proportional to strain |
| A. | elastic limit |
| B. | proportional limit |
| C. | yield stress |
| D. | all of the above |
| Answer» C. yield stress | |
| 665. |
for calculating a proof stress, a parallel line is drawn at |
| A. | 0.1% of yield elongation |
| B. | 0.2% of total elongation |
| C. | 0.2% of yield elongation |
| D. | 0.1% of total elongation |
| Answer» C. 0.2% of yield elongation | |
| 666. |
                   property is not directly shown on the stress strain curve |
| A. | ductility |
| B. | malleability |
| C. | stiffness |
| D. | all of the above |
| Answer» E. | |
| 667. |
               is the stress at which material shows a specified amount of plastic deformation |
| A. | yirld point stress |
| B. | proportional limit |
| C. | proof stress |
| D. | ultimate tensile stress |
| Answer» D. ultimate tensile stress | |
| 668. |
in tensile stress, necking occurs at a point where |
| A. | (dσt/det) = et |
| B. | (det/dσt) = σt |
| C. | (det/dσt) = et |
| D. | (dσt/det) = σt |
| Answer» E. | |
| 669. |
the relation between true stress and engineering stress is |
| A. | σe=σt(1+e) |
| B. | σt=σe(1+e) |
| C. | σt=σe(1-e) |
| D. | σe=2σt(1+e) |
| Answer» C. σt=σe(1-e) | |
| 670. |
the material which does not show the predefined yield stress, the yield stress can be determined by |
| A. | prone stress method |
| B. | proof stress method |
| C. | any one of above |
| D. | none of the above |
| Answer» C. any one of above | |
| 671. |
the tests which come under the group of destructive tests are |
| A. | tensile and compressive test |
| B. | shear and bend test |
| C. | impact and fatigue test |
| D. | any one of above |
| Answer» E. | |
| 672. |
the relation between true strain and engineering strain is |
| A. | e=ln(1+et) |
| B. | et=ln(1+2e) |
| C. | et=ln(1-2e) |
| D. | et=ln(1+e) |
| Answer» E. | |
| 673. |
the test which come under the group of destructive tests is |
| A. | dye penetrant test |
| B. | ultrasonic test |
| C. | eddy current test |
| D. | none of the above |
| Answer» E. | |
| 674. |
during the tensile test, the length of specimen and its cross section area |
| A. | increases, increases |
| B. | decreases, increases |
| C. | increases, decreases |
| D. | decreases, decreases |
| Answer» D. decreases, decreases | |
| 675. |
in engineering stress we consider |
| A. | original cross section |
| B. | instantaneou s cross section |
| C. | cross section after the test |
| D. | none of the above |
| Answer» B. instantaneou s cross section | |
| 676. |
the graphical representation of results of tensile test is known as |
| A. | stress strain curve |
| B. | s-n curve |
| C. | creep curve |
| D. | none of the above |
| Answer» B. s-n curve | |
| 677. |
any sudden change in cross section leads to the formaiton of area |
| A. | stiff |
| B. | stres concentratio n |
| C. | any one of above |
| D. | none of the above |
| Answer» C. any one of above | |
| 678. |
all the calculations in tensile test are carried out on a particular distance which is called as |
| A. | gauge length |
| B. | gause length |
| C. | gase length |
| D. | none of the above |
| Answer» B. gause length | |
| 679. |
after ultimate stress, stress goes on |
| A. | reducing |
| B. | increasing |
| C. | stabilised |
| D. | all of the above |
| Answer» B. increasing | |
| 680. |
dummy pointer on load - cell is used to indicate |
| A. | yield load |
| B. | breaking load |
| C. | ultimate load |
| D. | none of the above |
| Answer» D. none of the above | |
| 681. |
for measuring the elongation of specimen on UTM during tensile test is used |
| A. | durometer |
| B. | elastometer |
| C. | vernier |
| D. | extensomete r |
| Answer» E. | |
| 682. |
true stress is defiend as |
| A. | instantaneou s load / (original cross section area) |
| B. | applied load / (actual cross section area) |
| C. | applied load / (original cross section area) |
| D. | instantaneou s load / (original cross section area) |
| Answer» E. | |
| 683. |
A tensile test specimen has cross section |
| A. | square |
| B. | rectangular |
| C. | circular |
| D. | all of the above |
| Answer» E. | |
| 684. |
modulus of resilience is given as |
| A. | 2σ2/e |
| B. | σ2/e |
| C. | σ2/2e |
| D. | σ2/4e |
| Answer» D. σ2/4e | |
| 685. |
modulus of resilience is |
| A. | toughness / volume |
| B. | resilience / volume |
| C. | energy absorbed / volume |
| D. | stiffness / volume |
| Answer» D. stiffness / volume | |
| 686. |
engineering stress is defined as |
| A. | instantaneou s load / (original cross section area) |
| B. | applied load / (actual cross section area) |
| C. | applied load / (original cross section area) |
| D. | instantaneou s load / (actual cross section area) |
| Answer» D. instantaneou s load / (actual cross section area) | |
| 687. |
for tensile testing machine is used |
| A. | universal testing |
| B. | impact testing |
| C. | fatigue testing |
| D. | torsion testing |
| Answer» B. impact testing | |
| 688. |
materials like Al shows better |
| A. | ductility |
| B. | malleability |
| C. | toughness |
| D. | all of the above |
| Answer» E. | |
| 689. |
                 is the property of a material by which it can be drawin into wires |
| A. | ductility |
| B. | plasticity |
| C. | malleability |
| D. | toughness |
| Answer» B. plasticity | |
| 690. |
resistance of a material for its deformation is called as |
| A. | hardness |
| B. | toughness |
| C. | stiffness |
| D. | all of the above |
| Answer» D. all of the above | |
| 691. |
ductile material shows toughness |
| A. | low |
| B. | high |
| C. | medium |
| D. | none of the above |
| Answer» C. medium | |
| 692. |
brittle material shows toughness |
| A. | low |
| B. | high |
| C. | medium |
| D. | none of the above |
| Answer» B. high | |
| 693. |
modulus of toughness is |
| A. | toughness/ar ea |
| B. | toughness/vo lume |
| C. | toughness/wi dth |
| D. | toughness/le ngth |
| Answer» C. toughness/wi dth | |
| 694. |
toughness is defined as total energy absorbed by material in |
| A. | elastic region |
| B. | plastic region |
| C. | both of the above |
| D. | none of the above |
| Answer» D. none of the above | |
| 695. |
total area under stress-strain curve is called as |
| A. | toughness |
| B. | resilience |
| C. | malleability |
| D. | ductility |
| Answer» B. resilience | |
| 696. |
area under stress-strain curve in elastic region is called as |
| A. | resilience |
| B. | stiffness |
| C. | toughness |
| D. | modulus of elasticity |
| Answer» B. stiffness | |
| 697. |
material shows localised deformation after |
| A. | after yield point |
| B. | after uts |
| C. | before yield point |
| D. | before uts |
| Answer» C. before yield point | |
| 698. |
the material shows atrain at cnstant stress that point is known as |
| A. | yield stress |
| B. | ultimate tensile stress |
| C. | breaking stress |
| D. | all of the above |
| Answer» B. ultimate tensile stress | |
| 699. |
material obey's hooks law in region |
| A. | plastic deformation |
| B. | elastic deformation |
| C. | the region of change of elasticity to plasticity |
| D. | none of the above |
| Answer» C. the region of change of elasticity to plasticity | |
| 700. |
           is constant at the yield point |
| A. | strain |
| B. | stress |
| C. | temperature |
| D. | all of the above |
| Answer» C. temperature | |