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Dave’s Revision Notes

       STRUCTURES
         Outcome 4




                        Gary Plimer 2008
STRUCTURES Outcome 4



OUTCOME 4

When the students have completed this unit they should be able to:

 Use tabulated and graphical data to select materials
 Calculate factor of safety
 Consider the effect of the environment on structures.

Before you start this unit you should have an understanding of:

   Stress
   Strain
   Young’s Modulus
   Properties of materials.
STRUCTURES Outcome 4


FACTOR OF SAFETY

Most structures are extremely safe and well designed but due to unforeseen
  circumstances some structures fail or collapse. A structural engineer can
  never be absolutely certain that he/she has accounted for every possible
  type of load that will affect the structure. When a structure has failed, an
  investigation normally takes place to discover the reason for failure. The
  most common reasons include:

Overloading

This is when the load on the structure exceeds the value that was used during
   the design process. This type of failure may be due to the structure being
   used inappropriately, e.g. a man riding a child’s bike, or because the
   circumstances have changed since the original design. This may overload
   the structure beyond its design limit.

                                              Continued
STRUCTURES Outcome 4

The most dangerous cause for a sudden change in loading on a structure is
probably the weather. This is because of its unpredictable nature.


Material/Joint Failure

The material within the structure may fail if it is not of consistent quality or
   because it has deteriorated due to the working environment of the
   structure. We could never guarantee the performance of natural materials
   such as wood as they all contain natural defects such as knots, shakes
   etc. Some materials are susceptible to particular conditions, for example
   wood swells up as it absorbs moisture, mild steel rusts due to oxygen and
   water.
The joints used within the structure may fail because they are inappropriate
   and cannot support the load, or if they have been poorly made. This is
   particularly relevant with techniques such as welding. The welds on large
   structures are usually x-rayed in order to detect any defects.
STRUCTURES Outcome 4


Fatigue

It is difficult to predict exactly when a structure will fail. Repeated loading and
     unloading of a structure will wear down the material’s resistance to breaking
     and eventually it will fail. This may even be the case if the load remains
     within the maximum used in the original design calculations. The principle
     of fatigue can be demonstrated by bending a paper clip backwards and
     forwards. The paper clip will not snap the first time, or probably the second.
     After that we are unsure just when the paper clip will fail. Each time we
     bend it we are not applying any greater a force but eventually the paper clip
     snaps.
STRUCTURES Outcome 4


Applying a Factor of Safety

Depending on the performance criteria which a structure must meet; a
factor of safety will be applied to the design. Factors of safety vary from
one structure to another, depending on the consequences of failure. The
factor of safety applied to a nuclear power station is much higher than
that for a conventional power station because the implications of
structural failure are far more serious.

The following points affect the decision on the factor of safety:

1.   The value of the maximum load and accuracy of calculations.
2.   The type of load on the structure.
3.   The reliability/quality of the material.
4.   The effect of corrosion or wear on the dimensions of the structure.
5.   Errors during manufacture or construction.
6.   The consequences of failure.
STRUCTURES Outcome 4

Calculating Factor of Safety

We can apply a factor of safety to a structure in one of two ways. The first is
in terms of the loading the structure can withstand and the second is in
terms of the stress within the structure.



                                UltimateLoad
             FactorofSafety =
                              SafeWorkingLoad

                                UltimateStress
             FactorofSafety =
                              SafeWorkingStress
STRUCTURES Outcome 4

Worked example: Factor of Safety

The maximum ultimate tensile stress for aluminium is 300 N/mm2. If the
working stress on a component is 50 N/mm2, calculate the factor of safety
applied in the design of the component.


                                     UltimateStress
                  FactorofSafety =
                                   SafeWorkingStress

                                     300
                  FactorofSafety =
                                     50

                  FactorofSafety = 6
STRUCTURES Outcome 4

ACCESSING TABULATED DATA

Most commonly used materials have been tested exhaustively and the test data is
available in British Standards publications. In the course of your work in
Technological Studies you will be required to use extracts from these publications in
the same way an engineer might.
                 Material              Young's    Yield Stress     Ultimate         Ultimate
                                       Modulus       N/mm2       Tensile Stress   Compressive
                                       kN/mm2                       N/mm2           Stress
                                                                                     N/mm2
         Mild Steel                      196           220             430             430
         Stainless Steel                190-200      286-500        760-1280         460-540
         Low-alloy steel                200-207     500-1980        680-2400        680-2400
         Cast iron                       120            -            120-160         600-900
         Aluminium alloy                  70           250             300             300
         Soft Brass                      100            50              80             280
         Cast Bronze                     120           150             300              -
         Titanium alloy                  110           950            1000            1000
         Nickel alloys                  130-234     200-1600        400-2000        400-2000
         Concrete (steel reinforced)     45-50          -               -              100
STRUCTURES Outcome 4

ACCESSING TABULATED DATA

Most commonly used materials have been tested exhaustively and the test data is
available in British Standards publications. In the course of your work in
Technological Studies you will be required to use extracts from these publications in
the same way an engineer might.
                 Material              Young's    Yield Stress     Ultimate         Ultimate
                                       Modulus       N/mm2       Tensile Stress   Compressive
                                       kN/mm2                       N/mm2           Stress
                                                                                     N/mm2
         Mild Steel                      196           220             430             430
         Stainless Steel                190-200      286-500        760-1280         460-540
         Low-alloy steel                200-207     500-1980        680-2400        680-2400
         Cast iron                       120            -            120-160         600-900
         Aluminium alloy                  70           250             300             300
         Soft Brass                      100            50              80             280
         Cast Bronze                     120           150             300              -
         Titanium alloy                  110           950            1000            1000
         Nickel alloys                  130-234     200-1600        400-2000        400-2000
         Concrete (steel reinforced)     45-50          -               -              100

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Structures Material Properties Guide

  • 1. Dave’s Revision Notes STRUCTURES Outcome 4 Gary Plimer 2008
  • 2. STRUCTURES Outcome 4 OUTCOME 4 When the students have completed this unit they should be able to:  Use tabulated and graphical data to select materials  Calculate factor of safety  Consider the effect of the environment on structures. Before you start this unit you should have an understanding of:  Stress  Strain  Young’s Modulus  Properties of materials.
  • 3. STRUCTURES Outcome 4 FACTOR OF SAFETY Most structures are extremely safe and well designed but due to unforeseen circumstances some structures fail or collapse. A structural engineer can never be absolutely certain that he/she has accounted for every possible type of load that will affect the structure. When a structure has failed, an investigation normally takes place to discover the reason for failure. The most common reasons include: Overloading This is when the load on the structure exceeds the value that was used during the design process. This type of failure may be due to the structure being used inappropriately, e.g. a man riding a child’s bike, or because the circumstances have changed since the original design. This may overload the structure beyond its design limit. Continued
  • 4. STRUCTURES Outcome 4 The most dangerous cause for a sudden change in loading on a structure is probably the weather. This is because of its unpredictable nature. Material/Joint Failure The material within the structure may fail if it is not of consistent quality or because it has deteriorated due to the working environment of the structure. We could never guarantee the performance of natural materials such as wood as they all contain natural defects such as knots, shakes etc. Some materials are susceptible to particular conditions, for example wood swells up as it absorbs moisture, mild steel rusts due to oxygen and water. The joints used within the structure may fail because they are inappropriate and cannot support the load, or if they have been poorly made. This is particularly relevant with techniques such as welding. The welds on large structures are usually x-rayed in order to detect any defects.
  • 5. STRUCTURES Outcome 4 Fatigue It is difficult to predict exactly when a structure will fail. Repeated loading and unloading of a structure will wear down the material’s resistance to breaking and eventually it will fail. This may even be the case if the load remains within the maximum used in the original design calculations. The principle of fatigue can be demonstrated by bending a paper clip backwards and forwards. The paper clip will not snap the first time, or probably the second. After that we are unsure just when the paper clip will fail. Each time we bend it we are not applying any greater a force but eventually the paper clip snaps.
  • 6. STRUCTURES Outcome 4 Applying a Factor of Safety Depending on the performance criteria which a structure must meet; a factor of safety will be applied to the design. Factors of safety vary from one structure to another, depending on the consequences of failure. The factor of safety applied to a nuclear power station is much higher than that for a conventional power station because the implications of structural failure are far more serious. The following points affect the decision on the factor of safety: 1. The value of the maximum load and accuracy of calculations. 2. The type of load on the structure. 3. The reliability/quality of the material. 4. The effect of corrosion or wear on the dimensions of the structure. 5. Errors during manufacture or construction. 6. The consequences of failure.
  • 7. STRUCTURES Outcome 4 Calculating Factor of Safety We can apply a factor of safety to a structure in one of two ways. The first is in terms of the loading the structure can withstand and the second is in terms of the stress within the structure. UltimateLoad FactorofSafety = SafeWorkingLoad UltimateStress FactorofSafety = SafeWorkingStress
  • 8. STRUCTURES Outcome 4 Worked example: Factor of Safety The maximum ultimate tensile stress for aluminium is 300 N/mm2. If the working stress on a component is 50 N/mm2, calculate the factor of safety applied in the design of the component. UltimateStress FactorofSafety = SafeWorkingStress 300 FactorofSafety = 50 FactorofSafety = 6
  • 9. STRUCTURES Outcome 4 ACCESSING TABULATED DATA Most commonly used materials have been tested exhaustively and the test data is available in British Standards publications. In the course of your work in Technological Studies you will be required to use extracts from these publications in the same way an engineer might. Material Young's Yield Stress Ultimate Ultimate Modulus N/mm2 Tensile Stress Compressive kN/mm2 N/mm2 Stress N/mm2 Mild Steel 196 220 430 430 Stainless Steel 190-200 286-500 760-1280 460-540 Low-alloy steel 200-207 500-1980 680-2400 680-2400 Cast iron 120 - 120-160 600-900 Aluminium alloy 70 250 300 300 Soft Brass 100 50 80 280 Cast Bronze 120 150 300 - Titanium alloy 110 950 1000 1000 Nickel alloys 130-234 200-1600 400-2000 400-2000 Concrete (steel reinforced) 45-50 - - 100
  • 10. STRUCTURES Outcome 4 ACCESSING TABULATED DATA Most commonly used materials have been tested exhaustively and the test data is available in British Standards publications. In the course of your work in Technological Studies you will be required to use extracts from these publications in the same way an engineer might. Material Young's Yield Stress Ultimate Ultimate Modulus N/mm2 Tensile Stress Compressive kN/mm2 N/mm2 Stress N/mm2 Mild Steel 196 220 430 430 Stainless Steel 190-200 286-500 760-1280 460-540 Low-alloy steel 200-207 500-1980 680-2400 680-2400 Cast iron 120 - 120-160 600-900 Aluminium alloy 70 250 300 300 Soft Brass 100 50 80 280 Cast Bronze 120 150 300 - Titanium alloy 110 950 1000 1000 Nickel alloys 130-234 200-1600 400-2000 400-2000 Concrete (steel reinforced) 45-50 - - 100