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'''Steel in fire''' describes | '''Steel in fire''' describes the heating, expansion and loss of mechanical performance of steel members exposed to fire. Steel can remain noncombustible while its strength and stiffness decrease. Structural performance therefore depends on temperature, loading, geometry, protection and support conditions, rather than combustibility alone.<ref name="KH_1-157">Kodur and Harmathy (2002), p. 1-157.</ref><ref name="M_4-209">Milke (2002), p. 4-209.</ref><ref name="M_4-211_4-212">Milke (2002), pp. 4-211–4-212.</ref> | ||
Assessment connects three stages: defining the fire exposure, calculating heat transfer into the steel and evaluating structural response. The gas temperature is an input to this sequence, not automatically the temperature of the member. Exposed surface, steel mass and protection determine how rapidly the member heats, while mechanical properties determine the consequences.<ref name="M_4-209" /><ref name="M_4-222_4-224">Milke (2002), pp. 4-222–4-224.</ref> | |||
A standard furnace exposure provides one basis for comparing protected and unprotected assemblies. A natural fire requires its own description of the thermal environment. Neither approach supplies one failure temperature for every steel product or structural system. The selected endpoint must remain connected to the load and conditions it represents.<ref name="VR_8.6">Van Rossum (2027), §8.6.</ref><ref name="KH_1-163">Kodur and Harmathy (2002), p. 1-163.</ref> | |||
== | == From fire exposure to steel temperature == | ||
The fire environment supplies heat to the surface of an exposed member. Radiation transfers energy from flames and hot surroundings, while convection transfers energy between the gases and the surface. Conduction then redistributes that energy within the steel. The member temperature follows this combined heat balance rather than simply equalling the surrounding gas temperature.<ref name="M_4-209" /><ref name="M_4-222">Milke (2002), p. 4-222.</ref> | |||
The exposure history must therefore be defined before a heating calculation can begin. A furnace curve supplies one repeatable history, while a natural compartment fire develops according to the fuel, ventilation and enclosure. Heat release rate and gas temperature are different quantities within that description. Van Rossum treats standard temperature curves as prescribed exposures, rather than predictions of every room fire.<ref name="VR_8.6" /> | |||
The exposed faces also matter. A column surrounded by fire receives a different boundary condition from a beam connected to a concrete slab. The slab can shield the upper part of the beam and take heat from it. Milke explains that these effects can create appreciable temperature differences between the lower and upper flanges.<ref name="M_4-223_4-224">Milke (2002), pp. 4-223–4-224.</ref> | |||
A thermal model can treat the member as uniformly hot or calculate a temperature distribution. The first approach is simpler and can suit some exposed sections. The second becomes relevant when temperature gradients affect the structural response. Choosing between them depends on the exposure, section and purpose of the calculation.<ref name="M_4-222_4-224" /> | |||
== | == Geometry and section factor == | ||
[[ | [[Section factor]] relates the heated surface to the amount of steel being heated. For a member with a constant cross-section, the heated perimeter divided by the cross-sectional area expresses this relationship. More heated perimeter per unit area generally gives a greater heating response under otherwise equal conditions. The comparison concerns exposure and thermal storage together.<ref name="M_4-222_4-224" /> | ||
Milke also uses the inverse form: mass per unit length divided by heated perimeter. Its SI unit is kilograms per square metre. A large value represents more steel mass behind each unit of heated surface and therefore greater thermal storage. Confusing this ratio with the perimeter-to-area section factor reverses the interpretation of which section heats faster.<ref name="M_4-219">Milke (2002), p. 4-219.</ref><ref name="M_4-222_4-224" /> | |||
[[ | [[File:fse-steel-in-fire-v1.svg|thumb|upright=1.5|alt=Two steel sections with different exposed perimeters and masses receiving the same nominal heat flux.|Section geometry affects steel heating. Based on Milke (2002), pp. 4-222–4-224.]] | ||
Protection can alter the relevant heated boundary. An insulating enclosure around a section need not follow every recess of the steel profile. Its thermal resistance and exposed perimeter form part of the protected-member model. The geometry used for an unprotected contour cannot automatically describe an enclosing board system.<ref name="M_4-213_4-214">Milke (2002), pp. 4-213–4-214.</ref><ref name="M_4-223">Milke (2002), p. 4-223.</ref> | |||
Milke | Shielding by adjacent construction likewise changes the surface receiving heat. Milke provides separate perimeter diagrams for different arrangements and connections to slabs. These diagrams distinguish steel area from the boundary exposed to the thermal environment. The resulting section factor describes a particular exposure configuration, rather than a permanent property of the section designation.<ref name="M_4-223" /> | ||
== | The two geometry ratios can be converted through density. Milke's steel density of 7,860 kg/m³ divided by the example mass-to-perimeter ratio of 39.3 kg/m² gives 200 m⁻¹. This is the corresponding heated-perimeter-to-area ratio for that example. The conversion leaves the physical section unchanged while expressing the same thermal-storage relationship in another form.<ref name="M_4-211">Milke (2002), p. 4-211.</ref><ref name="M_4-219" /><ref name="M_4-224">Milke (2002), p. 4-224.</ref> | ||
The conversion also provides a dimensional check. A perimeter divided by an area has units of inverse metres, whereas mass divided by heated area has units of kilograms per square metre. Values expressed in these units cannot be substituted directly for each other. The intervening density and the direction of the ratio determine their relationship.<ref name="M_4-222_4-224" /> | |||
== A simplified heating calculation == | |||
In a lumped-capacity model, the steel is assumed to have one temperature throughout its section. The heat entering over a short interval increases the energy stored in the steel. Dividing the incoming heat by the steel's heat capacity gives the temperature increment. Milke expresses the model using the mass-to-heated-perimeter ratio.<ref name="M_4-222" /> | |||
<math display="block">\Delta T_s=\frac{h_{\mathrm{tot}}}{c_s(m'/P)}(T_g-T_s)\Delta t</math> | |||
= | {| class="wikitable" | ||
! Symbol !! Description !! Unit | |||
|- | |||
| <math>\Delta T_s</math> || Steel temperature increment || K | |||
|- | |||
| <math>h_{\mathrm{tot}}</math> || Combined convection and linearised radiation coefficient || W/(m²·K) | |||
|- | |||
| <math>c_s</math> || Steel specific heat || J/(kg·K) | |||
|- | |||
| <math>m'</math> || Steel mass per unit member length || kg/m | |||
|- | |||
| <math>P</math> || Heated perimeter || m | |||
|- | |||
| <math>T_g,T_s</math> || Gas and steel temperatures || °C | |||
|- | |||
| <math>\Delta t</math> || Calculation interval || s | |||
|} | |||
The temperature difference in this equation has the same numerical value in kelvins and degrees Celsius. Radiation calculations used to determine the combined coefficient, however, require absolute temperatures. Milke separates the radiative and convective contributions and recommends short calculation intervals for this approximation. The equation is then applied repeatedly as the exposure and steel temperature change.<ref name="M_4-222_4-223">Milke (2002), pp. 4-222–4-223.</ref> | |||
A calculation of the convective contribution illustrates the role of the inputs. Milke gives a mass-to-perimeter ratio of 39.3 kg/m² for the contour of a W8 × 28 section. His A36 specific-heat expression gives 430 J/(kg·K) at 20 °C. Taking his example temperature level of 538 °C as an assumed gas temperature permits a simple initial-step comparison.<ref name="M_4-219" /><ref name="M_4-211" /><ref name="KH_1-163" /> | |||
With a convective coefficient of 25 W/(m²·K) and an interval of 10 s, the calculated convection-only rise is 7.7 K. The arithmetic uses the unrounded specific heat of 430.2 J/(kg·K). Radiation has deliberately been excluded from this component calculation, so 7.7 K is not a complete fire-heating prediction. The chosen gas temperature is an illustrative boundary condition, not a measured exposure for that section.<ref name="M_4-211" /><ref name="M_4-222_4-223" /> | |||
== Strength, stiffness and steel type == | |||
= | [[Strength reduction at elevated temperatures]] changes the load that a hot member can resist. Yield strength describes the onset of substantial permanent deformation in the adopted material model. The modulus of elasticity describes stiffness before that stage. A reduction in stiffness can increase deformation and affect stability even before the nominal yield-strength limit is reached.<ref name="M_4-211_4-212" /> | ||
The response is not identical for all steel products. Fleischmann and Buchanan distinguish hot-rolled reinforcing steel, cold-drawn prestressing steel and high-strength alloy steel. Their chapter presents different strength-temperature relationships for these materials. It also distinguishes yield strength from tensile strength where the relevant design property differs.<ref name="FB_4-240">Fleischmann and Buchanan (2002), p. 4-240.</ref> | |||
[[File:fse-steel-in-fire-v2.svg|thumb|upright=1.5|alt=Schematic strength curves for hot-rolled, prestressing and alloy steel that fall at different temperatures and cross.|Steel products respond differently to elevated temperature. Based on Fleischmann and Buchanan (2002), p. 4-240.]] | |||
Heating can also introduce creep, which is deformation that develops with time under sustained stress. Milke explains that creep depends on stress, heating rate and temperature. Some fire-design material relationships incorporate its effects implicitly. Combining data from incompatible test histories can therefore misrepresent the response even when the nominal steel temperature is the same.<ref name="M_4-212">Milke (2002), p. 4-212.</ref> | |||
Room-temperature strength consequently supplies only part of the required information. A thermal analysis determines where and when the steel heats. Temperature-dependent mechanical properties then connect those temperatures to the structural calculation. The assessment still requires the applied load and the relevant support conditions.<ref name="M_4-209" /><ref name="M_4-211_4-212" /> | |||
== | == Critical temperature and structural endpoints == | ||
[[Critical steel temperature]] is a temperature associated with an unacceptable structural condition under stated assumptions. It depends on the load to be supported and the material's remaining capacity. The concept can simplify a thermal calculation when those structural conditions have already been established. It does not replace them with a universal failure temperature.<ref name="KH_1-163" /><ref name="M_4-209" /> | |||
ASTM E119 | Kodur and Harmathy describe historical North American examples of 538 °C for structural steel, 593 °C for reinforcing steel and 426 °C for prestressing steel. The structural-steel example is associated with particular ASTM E119-related assumptions, including full design loading in the discussion of columns. These figures illustrate method-dependent endpoints. They do not represent melting temperatures or limits applicable to every steel member.<ref name="KH_1-163" /> | ||
[[File:fse-steel-in-fire-v3.svg|thumb|upright=1.5|alt=Critical-temperature examples 538, 593 and 426 °C for three steel uses.|Critical-temperature examples depend on steel use and method. Based on Kodur and Harmathy (2002), p. 1-163.]] | |||
Milke's description of A36 steel provides the mechanical context. At approximately 538 °C, its yield strength in the cited relationship is about 60% of the room-temperature value. The significance of that reduction depends on the stress already imposed on the member. A lightly loaded and a heavily loaded member need not reach their structural endpoints at the same temperature.<ref name="M_4-212" /> | |||
A | A temperature endpoint and a structural endpoint therefore answer related questions. The thermal calculation can determine when a specified temperature is reached. A structural calculation evaluates the resulting stresses, deformation and capacity under the adopted loading and restraint. Where a temperature criterion is used, its connection to those structural conditions remains part of the method.<ref name="M_4-209" /><ref name="M_4-222" /> | ||
== Expansion, restraint and structural response == | |||
Steel expands as its temperature rises. If supports or surrounding construction limit that movement, [[Restrained thermal expansion]] changes the forces and deformations within the system. The member then responds to more than its original mechanical loading. Milke consequently includes thermal expansion and end conditions in the structural assessment.<ref name="M_4-209_4-211">Milke (2002), pp. 4-209–4-211.</ref> | |||
Test restraint is a defined condition rather than an informal description of a connection. Milke reproduces historical ASTM examples distinguishing different floor and framing arrangements. The classification considers how the surrounding structure resists movement. A restrained test result therefore requires interpretation in relation to the proposed construction and its actual boundaries.<ref name="M_4-210_4-211">Milke (2002), pp. 4-210–4-211.</ref> | |||
Temperature gradients add another complication. A beam beneath a slab can have a hotter lower flange and a cooler upper flange. A uniform-temperature model does not explicitly describe that difference. Where the gradient affects the structural question, Milke identifies the need for a more suitable analytical approach.<ref name="M_4-223_4-224" /> | |||
[[Structural fire engineering]] combines these effects rather than treating steel temperature as a complete outcome. It uses the exposure to calculate temperatures, then applies temperature-dependent properties within a structural model. Loads, geometry and end conditions determine how the member responds. The required result may involve deformation and stability as well as a nominal strength comparison.<ref name="M_4-209_4-210">Milke (2002), pp. 4-209–4-210.</ref> | |||
== Protection systems and their behaviour == | |||
Protection reduces the rate of heat transfer into the steel. Milke describes insulating boards, spray-applied materials, concrete encasement and enclosing membranes. Their mechanisms and attachment details differ. The relevant evidence concerns the protected assembly, including the protection material and the way it remains attached during exposure.<ref name="M_4-212_4-214">Milke (2002), pp. 4-212–4-214.</ref> | |||
The | [[Intumescent material]] expands during heating to form an insulating layer. The change is part of the protective mechanism, so the layer cannot always be represented by its original thickness and properties. Van Rossum identifies swelling as one of several processes that change the heat-conduction path during fire. Milke includes intumescent products among spray-applied protection methods.<ref name="VR_5.2">Van Rossum (2027), §5.2.</ref><ref name="M_4-214">Milke (2002), p. 4-214.</ref> | ||
Board systems rely on suitable enclosure and attachment. Milke specifically identifies the means of securing boards as a factor affecting assembly performance. Spray-applied products require properties such as adhesion, durability and uniform application. These considerations connect the material's thermal performance to its condition on the actual member.<ref name="M_4-212_4-214" /> | |||
Protection can also store heat. Milke distinguishes simplified models that neglect its heat capacity from models that include it. Gypsum and concrete protection are examples where that contribution can matter. Omitting the protection's thermal storage is therefore an assumption to assess, rather than a property of every protected-steel calculation.<ref name="M_4-223" /> | |||
A protected member can receive heat through the insulation while the insulation itself is warming. Part of the incoming energy then increases the protection's temperature instead of immediately heating the steel. Milke includes this storage in the denominator of a protected-member temperature-increment expression. The effect differs from thermal resistance, which describes the rate of energy transfer through the layer.<ref name="M_4-223" /> | |||
An intact thermal barrier also needs to survive handling and its surrounding environment. Milke includes bond strength, durability, weathering resistance and consistent application among relevant protection characteristics. These requirements concern maintaining the protective arrangement that the thermal model assumes. A conductivity value alone cannot establish whether the applied protection will retain that arrangement throughout service and exposure.<ref name="M_4-212" /> | |||
== Evidence and modelling limits == | |||
Empirical protection formulas are linked to the tests from which they were developed. Milke cautions that their ranges can be restricted by member shapes, protection thickness and other conditions. A result outside those ranges has a different evidential basis from a result within them. The fire exposure, loading and span also limit the applicability of test-based correlations.<ref name="M_4-209" /><ref name="M_4-219" /> | |||
A more detailed thermal calculation does not remove uncertainty in its inputs. Heating conditions, temperature-dependent material properties and insulation behaviour still affect the result. A structural calculation introduces additional assumptions about loads and restraint. The accuracy of the combined prediction depends on the relationship between all these stages.<ref name="M_4-209_4-210" /> | |||
Tests provide evidence about interactions that simplified models may omit. Milke emphasises their role in establishing material behaviour and checking protected assemblies. The resulting evidence describes the tested exposure and configuration. Its application to another member depends on whether the model represents the changes in geometry, heating and structural conditions.<ref name="M_4-210_4-211" /> | |||
== See also == | == See also == | ||
| Line 120: | Line 121: | ||
* [[Progressive collapse]] | * [[Progressive collapse]] | ||
* [[Tensile membrane action]] | * [[Tensile membrane action]] | ||
* [[ | * [[Fire resistance]] | ||
== Notes == | == Notes == | ||
| Line 128: | Line 129: | ||
== References == | == References == | ||
* Fleischmann, C., & Buchanan, A. (2002). Analytical methods for determining fire resistance of concrete members. In P. J. DiNenno (Ed.), ''SFPE handbook of fire protection engineering'' (3rd ed., pp. 4-239–4-256). National Fire Protection Association. | |||
* Kodur, V. K. R., & Harmathy, T. Z. (2002). Properties of building materials. In P. J. DiNenno (Ed.), ''SFPE handbook of fire protection engineering'' (3rd ed., pp. 1-155–1-181). National Fire Protection Association. | |||
* Fleischmann, C., & Buchanan, A. (2002). Analytical methods for determining fire resistance of concrete members. In P. J. DiNenno (Ed.), ''SFPE handbook of fire protection engineering'' (3rd ed.). National Fire Protection Association. | * Milke, J. A. (2002). Analytical methods for determining fire resistance of steel members. In P. J. DiNenno (Ed.), ''SFPE handbook of fire protection engineering'' (3rd ed., pp. 4-209–4-238). National Fire Protection Association. | ||
* Kodur, V. K. R., & Harmathy, T. Z. (2002). Properties of building materials. In P. J. DiNenno (Ed.), ''SFPE handbook of fire protection engineering'' (3rd ed. | |||
* Milke, J. A. (2002). Analytical methods for determining fire resistance of steel members. In P. J. DiNenno (Ed.), ''SFPE handbook of fire protection engineering'' (3rd ed. | |||
* Van Rossum, E. (2027). ''Introduction to Fire Safety Engineering''. Fire Safety Academy. | * Van Rossum, E. (2027). ''Introduction to Fire Safety Engineering''. Fire Safety Academy. | ||
[[Category:Structural Fire Engineering]] | [[Category:Structural Fire Engineering]] | ||
Revision as of 18:54, 2 November 2026
Steel in fire describes the heating, expansion and loss of mechanical performance of steel members exposed to fire. Steel can remain noncombustible while its strength and stiffness decrease. Structural performance therefore depends on temperature, loading, geometry, protection and support conditions, rather than combustibility alone.[1][2][3]
Assessment connects three stages: defining the fire exposure, calculating heat transfer into the steel and evaluating structural response. The gas temperature is an input to this sequence, not automatically the temperature of the member. Exposed surface, steel mass and protection determine how rapidly the member heats, while mechanical properties determine the consequences.[2][4]
A standard furnace exposure provides one basis for comparing protected and unprotected assemblies. A natural fire requires its own description of the thermal environment. Neither approach supplies one failure temperature for every steel product or structural system. The selected endpoint must remain connected to the load and conditions it represents.[5][6]
From fire exposure to steel temperature
The fire environment supplies heat to the surface of an exposed member. Radiation transfers energy from flames and hot surroundings, while convection transfers energy between the gases and the surface. Conduction then redistributes that energy within the steel. The member temperature follows this combined heat balance rather than simply equalling the surrounding gas temperature.[2][7]
The exposure history must therefore be defined before a heating calculation can begin. A furnace curve supplies one repeatable history, while a natural compartment fire develops according to the fuel, ventilation and enclosure. Heat release rate and gas temperature are different quantities within that description. Van Rossum treats standard temperature curves as prescribed exposures, rather than predictions of every room fire.[5]
The exposed faces also matter. A column surrounded by fire receives a different boundary condition from a beam connected to a concrete slab. The slab can shield the upper part of the beam and take heat from it. Milke explains that these effects can create appreciable temperature differences between the lower and upper flanges.[8]
A thermal model can treat the member as uniformly hot or calculate a temperature distribution. The first approach is simpler and can suit some exposed sections. The second becomes relevant when temperature gradients affect the structural response. Choosing between them depends on the exposure, section and purpose of the calculation.[4]
Geometry and section factor
Section factor relates the heated surface to the amount of steel being heated. For a member with a constant cross-section, the heated perimeter divided by the cross-sectional area expresses this relationship. More heated perimeter per unit area generally gives a greater heating response under otherwise equal conditions. The comparison concerns exposure and thermal storage together.[4]
Milke also uses the inverse form: mass per unit length divided by heated perimeter. Its SI unit is kilograms per square metre. A large value represents more steel mass behind each unit of heated surface and therefore greater thermal storage. Confusing this ratio with the perimeter-to-area section factor reverses the interpretation of which section heats faster.[9][4]
Protection can alter the relevant heated boundary. An insulating enclosure around a section need not follow every recess of the steel profile. Its thermal resistance and exposed perimeter form part of the protected-member model. The geometry used for an unprotected contour cannot automatically describe an enclosing board system.[10][11]
Shielding by adjacent construction likewise changes the surface receiving heat. Milke provides separate perimeter diagrams for different arrangements and connections to slabs. These diagrams distinguish steel area from the boundary exposed to the thermal environment. The resulting section factor describes a particular exposure configuration, rather than a permanent property of the section designation.[11]
The two geometry ratios can be converted through density. Milke's steel density of 7,860 kg/m³ divided by the example mass-to-perimeter ratio of 39.3 kg/m² gives 200 m⁻¹. This is the corresponding heated-perimeter-to-area ratio for that example. The conversion leaves the physical section unchanged while expressing the same thermal-storage relationship in another form.[12][9][13]
The conversion also provides a dimensional check. A perimeter divided by an area has units of inverse metres, whereas mass divided by heated area has units of kilograms per square metre. Values expressed in these units cannot be substituted directly for each other. The intervening density and the direction of the ratio determine their relationship.[4]
A simplified heating calculation
In a lumped-capacity model, the steel is assumed to have one temperature throughout its section. The heat entering over a short interval increases the energy stored in the steel. Dividing the incoming heat by the steel's heat capacity gives the temperature increment. Milke expresses the model using the mass-to-heated-perimeter ratio.[7]
| Symbol | Description | Unit |
|---|---|---|
| Steel temperature increment | K | |
| Combined convection and linearised radiation coefficient | W/(m²·K) | |
| Steel specific heat | J/(kg·K) | |
| Steel mass per unit member length | kg/m | |
| Heated perimeter | m | |
| Gas and steel temperatures | °C | |
| Calculation interval | s |
The temperature difference in this equation has the same numerical value in kelvins and degrees Celsius. Radiation calculations used to determine the combined coefficient, however, require absolute temperatures. Milke separates the radiative and convective contributions and recommends short calculation intervals for this approximation. The equation is then applied repeatedly as the exposure and steel temperature change.[14]
A calculation of the convective contribution illustrates the role of the inputs. Milke gives a mass-to-perimeter ratio of 39.3 kg/m² for the contour of a W8 × 28 section. His A36 specific-heat expression gives 430 J/(kg·K) at 20 °C. Taking his example temperature level of 538 °C as an assumed gas temperature permits a simple initial-step comparison.[9][12][6]
With a convective coefficient of 25 W/(m²·K) and an interval of 10 s, the calculated convection-only rise is 7.7 K. The arithmetic uses the unrounded specific heat of 430.2 J/(kg·K). Radiation has deliberately been excluded from this component calculation, so 7.7 K is not a complete fire-heating prediction. The chosen gas temperature is an illustrative boundary condition, not a measured exposure for that section.[12][14]
Strength, stiffness and steel type
Strength reduction at elevated temperatures changes the load that a hot member can resist. Yield strength describes the onset of substantial permanent deformation in the adopted material model. The modulus of elasticity describes stiffness before that stage. A reduction in stiffness can increase deformation and affect stability even before the nominal yield-strength limit is reached.[3]
The response is not identical for all steel products. Fleischmann and Buchanan distinguish hot-rolled reinforcing steel, cold-drawn prestressing steel and high-strength alloy steel. Their chapter presents different strength-temperature relationships for these materials. It also distinguishes yield strength from tensile strength where the relevant design property differs.[15]
Heating can also introduce creep, which is deformation that develops with time under sustained stress. Milke explains that creep depends on stress, heating rate and temperature. Some fire-design material relationships incorporate its effects implicitly. Combining data from incompatible test histories can therefore misrepresent the response even when the nominal steel temperature is the same.[16]
Room-temperature strength consequently supplies only part of the required information. A thermal analysis determines where and when the steel heats. Temperature-dependent mechanical properties then connect those temperatures to the structural calculation. The assessment still requires the applied load and the relevant support conditions.[2][3]
Critical temperature and structural endpoints
Critical steel temperature is a temperature associated with an unacceptable structural condition under stated assumptions. It depends on the load to be supported and the material's remaining capacity. The concept can simplify a thermal calculation when those structural conditions have already been established. It does not replace them with a universal failure temperature.[6][2]
Kodur and Harmathy describe historical North American examples of 538 °C for structural steel, 593 °C for reinforcing steel and 426 °C for prestressing steel. The structural-steel example is associated with particular ASTM E119-related assumptions, including full design loading in the discussion of columns. These figures illustrate method-dependent endpoints. They do not represent melting temperatures or limits applicable to every steel member.[6]
Milke's description of A36 steel provides the mechanical context. At approximately 538 °C, its yield strength in the cited relationship is about 60% of the room-temperature value. The significance of that reduction depends on the stress already imposed on the member. A lightly loaded and a heavily loaded member need not reach their structural endpoints at the same temperature.[16]
A temperature endpoint and a structural endpoint therefore answer related questions. The thermal calculation can determine when a specified temperature is reached. A structural calculation evaluates the resulting stresses, deformation and capacity under the adopted loading and restraint. Where a temperature criterion is used, its connection to those structural conditions remains part of the method.[2][7]
Expansion, restraint and structural response
Steel expands as its temperature rises. If supports or surrounding construction limit that movement, Restrained thermal expansion changes the forces and deformations within the system. The member then responds to more than its original mechanical loading. Milke consequently includes thermal expansion and end conditions in the structural assessment.[17]
Test restraint is a defined condition rather than an informal description of a connection. Milke reproduces historical ASTM examples distinguishing different floor and framing arrangements. The classification considers how the surrounding structure resists movement. A restrained test result therefore requires interpretation in relation to the proposed construction and its actual boundaries.[18]
Temperature gradients add another complication. A beam beneath a slab can have a hotter lower flange and a cooler upper flange. A uniform-temperature model does not explicitly describe that difference. Where the gradient affects the structural question, Milke identifies the need for a more suitable analytical approach.[8]
Structural fire engineering combines these effects rather than treating steel temperature as a complete outcome. It uses the exposure to calculate temperatures, then applies temperature-dependent properties within a structural model. Loads, geometry and end conditions determine how the member responds. The required result may involve deformation and stability as well as a nominal strength comparison.[19]
Protection systems and their behaviour
Protection reduces the rate of heat transfer into the steel. Milke describes insulating boards, spray-applied materials, concrete encasement and enclosing membranes. Their mechanisms and attachment details differ. The relevant evidence concerns the protected assembly, including the protection material and the way it remains attached during exposure.[20]
Intumescent material expands during heating to form an insulating layer. The change is part of the protective mechanism, so the layer cannot always be represented by its original thickness and properties. Van Rossum identifies swelling as one of several processes that change the heat-conduction path during fire. Milke includes intumescent products among spray-applied protection methods.[21][22]
Board systems rely on suitable enclosure and attachment. Milke specifically identifies the means of securing boards as a factor affecting assembly performance. Spray-applied products require properties such as adhesion, durability and uniform application. These considerations connect the material's thermal performance to its condition on the actual member.[20]
Protection can also store heat. Milke distinguishes simplified models that neglect its heat capacity from models that include it. Gypsum and concrete protection are examples where that contribution can matter. Omitting the protection's thermal storage is therefore an assumption to assess, rather than a property of every protected-steel calculation.[11]
A protected member can receive heat through the insulation while the insulation itself is warming. Part of the incoming energy then increases the protection's temperature instead of immediately heating the steel. Milke includes this storage in the denominator of a protected-member temperature-increment expression. The effect differs from thermal resistance, which describes the rate of energy transfer through the layer.[11]
An intact thermal barrier also needs to survive handling and its surrounding environment. Milke includes bond strength, durability, weathering resistance and consistent application among relevant protection characteristics. These requirements concern maintaining the protective arrangement that the thermal model assumes. A conductivity value alone cannot establish whether the applied protection will retain that arrangement throughout service and exposure.[16]
Evidence and modelling limits
Empirical protection formulas are linked to the tests from which they were developed. Milke cautions that their ranges can be restricted by member shapes, protection thickness and other conditions. A result outside those ranges has a different evidential basis from a result within them. The fire exposure, loading and span also limit the applicability of test-based correlations.[2][9]
A more detailed thermal calculation does not remove uncertainty in its inputs. Heating conditions, temperature-dependent material properties and insulation behaviour still affect the result. A structural calculation introduces additional assumptions about loads and restraint. The accuracy of the combined prediction depends on the relationship between all these stages.[19]
Tests provide evidence about interactions that simplified models may omit. Milke emphasises their role in establishing material behaviour and checking protected assemblies. The resulting evidence describes the tested exposure and configuration. Its application to another member depends on whether the model represents the changes in geometry, heating and structural conditions.[18]
See also
Notes
- ↑ Kodur and Harmathy (2002), p. 1-157.
- ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 Milke (2002), p. 4-209.
- ↑ 3.0 3.1 3.2 Milke (2002), pp. 4-211–4-212.
- ↑ 4.0 4.1 4.2 4.3 4.4 Milke (2002), pp. 4-222–4-224.
- ↑ 5.0 5.1 Van Rossum (2027), §8.6.
- ↑ 6.0 6.1 6.2 6.3 Kodur and Harmathy (2002), p. 1-163.
- ↑ 7.0 7.1 7.2 Milke (2002), p. 4-222.
- ↑ 8.0 8.1 Milke (2002), pp. 4-223–4-224.
- ↑ 9.0 9.1 9.2 9.3 Milke (2002), p. 4-219.
- ↑ Milke (2002), pp. 4-213–4-214.
- ↑ 11.0 11.1 11.2 11.3 Milke (2002), p. 4-223.
- ↑ 12.0 12.1 12.2 Milke (2002), p. 4-211.
- ↑ Milke (2002), p. 4-224.
- ↑ 14.0 14.1 Milke (2002), pp. 4-222–4-223.
- ↑ Fleischmann and Buchanan (2002), p. 4-240.
- ↑ 16.0 16.1 16.2 Milke (2002), p. 4-212.
- ↑ Milke (2002), pp. 4-209–4-211.
- ↑ 18.0 18.1 Milke (2002), pp. 4-210–4-211.
- ↑ 19.0 19.1 Milke (2002), pp. 4-209–4-210.
- ↑ 20.0 20.1 Milke (2002), pp. 4-212–4-214.
- ↑ Van Rossum (2027), §5.2.
- ↑ Milke (2002), p. 4-214.
References
- Fleischmann, C., & Buchanan, A. (2002). Analytical methods for determining fire resistance of concrete members. In P. J. DiNenno (Ed.), SFPE handbook of fire protection engineering (3rd ed., pp. 4-239–4-256). National Fire Protection Association.
- Kodur, V. K. R., & Harmathy, T. Z. (2002). Properties of building materials. In P. J. DiNenno (Ed.), SFPE handbook of fire protection engineering (3rd ed., pp. 1-155–1-181). National Fire Protection Association.
- Milke, J. A. (2002). Analytical methods for determining fire resistance of steel members. In P. J. DiNenno (Ed.), SFPE handbook of fire protection engineering (3rd ed., pp. 4-209–4-238). National Fire Protection Association.
- Van Rossum, E. (2027). Introduction to Fire Safety Engineering. Fire Safety Academy.