Structural Reviewer Part 2

31 Questions | Total Attempts: 410

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Structural Reviewer Part 2 - Quiz

Architecture Board exam


Questions and Answers
  • 1. 
    The strength reduction factor for flexure without tension
    • A. 

      0.85

    • B. 

      0.75

    • C. 

      0.70

    • D. 

      0.90

    • E. 

      None of the above

  • 2. 
    The strength reduction factor for axial tension and axial tension w/ flexure
    • A. 

      0.90

    • B. 

      0.85

    • C. 

      0.70

    • D. 

      0.75

    • E. 

      None of the above

  • 3. 
    The strength reduction factor for shear and torsion
    • A. 

      0.90

    • B. 

      0.75

    • C. 

      0.70

    • D. 

      0.60

    • E. 

      None of the sbove

  • 4. 
    The strength reduction factor for axial compression and axial compression with flexure for spiral reinforcement
    • A. 

      0.75

    • B. 

      0.60

    • C. 

      0.85

    • D. 

      0.90

  • 5. 
    The strength reduction factor for axial compression and axial compression with flexure for tie reinforcement
    • A. 

      0.75

    • B. 

      0.85

    • C. 

      0.70

    • D. 

      0.90

  • 6. 
    The strength reduction factor for bearing on concrete
    • A. 

      0.75

    • B. 

      0.70

    • C. 

      0.85

    • D. 

      0.90

  • 7. 
    The slenderness ratio L/r preferably should not exceed _____ for members whose design is based on COMPRESSIVE FORCE
    • A. 

      200

    • B. 

      300

    • C. 

      250

    • D. 

      400

  • 8. 
    The slenderness ratio L/r preferably should not exceed _____ for members whose design is based on TENSILE FORCE
    • A. 

      250

    • B. 

      200

    • C. 

      400

    • D. 

      300

  • 9. 
    The ratio L/r for lacing bars arranged in SINGLE system shall not exceed
    • A. 

      200mm

    • B. 

      300mm

    • C. 

      250mm

    • D. 

      140mm

  • 10. 
    The ratio L/r for lacing bars arranged in DOUBLE system shall not exceed
    • A. 

      140mm

    • B. 

      300mm

    • C. 

      200mm

    • D. 

      250mm

  • 11. 
    For members bent about their STRONG or WEAK AXES, members with compact sections where the flanges continuously connected to web, the allowable bending stress is 
    • A. 

      0.60 fy

    • B. 

      0.70 fy

    • C. 

      0.75 fy

    • D. 

      0.66 fy

  • 12. 
    For BOX type and TABULAR textural members that meet the non compact section requirements of section 502.6 the allowable bending stress is
    • A. 

      0.75 fy

    • B. 

      0.60 fy

    • C. 

      0.70 fy

    • D. 

      0.66 fy

  • 13. 
    The MAXIMUM UNIT STRESS permitted for a material in the design of a structural member. Also called ALLOWABLE UNIT STRESS, WORKING STRESS
    • A. 

      Maximum stress

    • B. 

      Ultimate stress

    • C. 

      Allowable stress

    • D. 

      Stress

  • 14. 
    A graphic representation of the relationship between unit stress values and the corresponding unit strains for a specific material
    • A. 

      Tensile Diagram

    • B. 

      Moment Diagram

    • C. 

      Ultimate strength Diagram

    • D. 

      Stress-Strain Diagram

  • 15. 
    The property of a material that enables it to DEFORM in response to an applied force and to recover its original size and shape upon removal force
    • A. 

      Elasticity

    • B. 

      Malleability

    • C. 

      Toughness

    • D. 

      Ductility

  • 16. 
    The property of the material that enables it to under go PLASTIC DEFORMATION after being stressed beyond the elastic limit and before rupturing.
    • A. 

      Toughness

    • B. 

      Ductility

    • C. 

      Malleability

    • D. 

      Elasticity

  • 17. 
    The property of a material that enables it to absorb energy before rupturing.
    • A. 

      Malleability

    • B. 

      Elasticity

    • C. 

      Toughness

    • D. 

      Ductility

  • 18. 
    The maximum stress than can be attained immediately before actual failure or rupture 
    • A. 

      Yield point

    • B. 

      Elastic limit

    • C. 

      Proportional limit

    • D. 

      Ultimate Strength

  • 19. 
    Maximum stress which the material springs back to the original length when the load is released
    • A. 

      Proportional Limit

    • B. 

      Elastic Limit

    • C. 

      Yield Point

    • D. 

      Ultimate Strength

  • 20. 
    The stress where in the deformation increases without any increase in load.
    • A. 

      Ultimate Strength

    • B. 

      Yield Point

    • C. 

      Proportional Limit

    • D. 

      Elastic Limit

  • 21. 
    The gradual deformation of a body produced by a continued application of stress or prolonged exposure to heat
    • A. 

      Creep

    • B. 

      Fatigue

    • C. 

      Strain

    • D. 

      Elastic Range

  • 22. 
    The act of stretching or state of being pulled apart, resulting in the elongation of an elastic body
    • A. 

      Compression

    • B. 

      Tension

    • C. 

      Stress

    • D. 

      Force

  • 23. 
    A tensile or compressive force acting along the longitudinal axis of a structural member and a the centroid of the cross section, producing axial stress without bending, torsion or shear also called AXIAL LOAD
    • A. 

      Axial Force

    • B. 

      Tensile Force

    • C. 

      Compressive Force

    • D. 

      Eccentric Force

  • 24. 
    The ratio of lateral strain to the corresponding longitudinal strain in an elastic body under longitudinal stress
    • A. 

      Slenderness ratio

    • B. 

      Poisson's Ratio

    • C. 

      Compressive Ratio

    • D. 

      Axial Ratio

  • 25. 
    The axial stress that develops at the cross section of an elastic body to resist the
    • A. 

      Tensile stress

    • B. 

      Compressive stress

    • C. 

      Stress

    • D. 

      Tension

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