Comparing LRFD & ASD Results Last Revised: 11/04/2014
LRFD and ASD loads are not directly comparable because they are used dierently dierently by the desi!n desi!n codes" LRFD loads are are !enerally !enerally compared to member or component S#R$%' (hereas ASD loads are compared to member or component allo(able values that are less than the )ull stren!th stren!th o) the member or or component" *n order to to determine (hich desi!n philosophy is more or less demandin! +i"e" results in lar!er members,members,- it is necessary to .un)actor. the load combinations usin! the material specic stren!th and allo(able stress reuirements" Also- there are times (hen you (ill no( the capacity o) a member relative to a limit state and (ant to no( (hat actual loads you can put on it" *n order to accomplish this tas you need to .turn around. around. the load combination euations and compute D- L- etc" #o accomplish this tas- you (ill need to no( the relative ma!nitudes o) the service load +i"e" actual applied ma!nitudes, ma!nitudes, components" #his tends to !et !et etraordinarily etraordinarily di3cult di3cult i) your member member has multiple load sources +i"e" a uni)orm load- a point load- etc",ho(ever i) you have a sin!le load source the tas is mana!eable" mana!eable" #his tet uses uses a service level level euivalent loadload- s-euiv +or s-e,- )or comparison o) LRFD LRFD and ASD loads" loads" #he euivalent euivalent service load is is taen to be the sum o) all service level load components etracted )rom a particular load combination euation" euation" #he net net section illustrates this concept usin! the reuirements o) the 15th edition o) the A*S6 Steel 6onstruction 7anual"
Converting Load Combinations to a Comparable Equivalent Load #he typical stren!th stren!th based limit state statement statement taes taes the )orm: )orm: LRFD
ASD
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u 8 φn
a 8 n/ Ω
9here u and a are values o) desi!n loads that have been computed usin! the load combination euations and the terms on the ri!ht side o) each euation represent represent the capacity o) the member" For eampleeample- let us assume that (e no( the aial )orce capacity o) a tension member and that the applied dead load euals the live load and the seismic seismic load is t(ice the dead dead load" *n other (ords(ords- the load consists o) one part dead load- one part live load- and t(o parts seismic load For this situation- (e introduce the uantity s-euiv (hich is the sum o) the service level level load components" components" For our our eample: eample: s-euiv D ; L ; $ 9here • D 1/4 s-euiv 0"2< s-euiv • L 1/4 s-euiv 0"2< s-euiv • $ 2/4 s-euiv 0"<0 s-euiv
#he uantities u and a can be related to s-euiv by a composite load factor (CLF) that is derived )rom the load combination euations and the relative values o) the individual load components" LRFD
ASD
u 6LFLRFD=s-euiv
a 6LFASD=s-euiv
#he composite load )actor is then then computed )or each each load case" #he lar!est 6LF (ill be )rom the controllin! load case"
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2" u 1"2+0"2< s-euiv, ; 1">+0"2< s-euiv, 0"?0 s-euiv 5" u 1"2+0"2< s-euiv, ; 0"<+0"2< s-euiv, 0"42< s-euiv 4" u 1"2+0"2< s-euiv, ; 0"<+0"2< s-euiv, 0"42< s-euiv <" u 1"2+0"2< s-euiv, ; 1"0+0"<0 s-euiv, ; 0"<+0"2< s-euiv, 0"@2< s-euiv >" u 0"@+0"2< s-euiv, ; 1"0+0"<0 s-euiv, 0"?2< s-euiv #he controllin! controllin! 6LFLRFD in this case is )rom LRFD L6< and is 0"@2<" 9ith the 6LFLRFD (e can no( nd the allo(able ma!nitudes o) D- Land $" 7aimum u 0"@2< s-euiv 8 φn s-euiv 8 +φn,/0"@2< From this (e can compute the service level ma!nitudes )or D- L- and $- by substitutin! +φn,/0"@2
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?" a 0">0+0"2< s-euiv, 0">0 s-euiv C" a 0">0+0"2< s-euiv, ; 0"?0+0"<0 s-euiv, 0"<0 s-euiv
#he controllin! controllin! 6LFASD in this case is )rom ASD L6> and is 0"?0" 9ith the 6LFASD (e can no( nd the allo(able ma!nitudes o) D- L- and $" 0"?0 s-euiv 8 n/ Ω s-euiv 8 +n/ Ω,/0"?0 From this (e can compute the service level ma!nitudes )or D- L- and $: D 8 0"2< +n/ Ω,/0"?0 L 8 0"2< + n/ Ω,/0"?0 $ 8 0"<0 + n/ Ω,/0"?0 #he controllin! controllin! composite load )actor- 6LFASD- can be easily computed usin! the same spreadsheet spreadsheet you (ould use )or computin! all the load combinations simply by puttin! in the th e coe3cients )or the various load types in a sin!le load source column"
Comparing ASD vs LRFD Loads 6onsider a steel tension member that has a nominal aial capacityn- and is subected subected to a combination combination o) dead and live loads" 9e (ill use φ 0"@ and Ω 1">? )or no(" #he LRFD and ASD )actored )actored loads are are not directly directly comparable comparable as the combination euations euations use dierent dierent load )actors )actors in each case" 9e can compare them at service levels by computin! an euivalent service load )rom each combination"
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ASD
#he controllin! controllin! ASD load combination combination euation euation in this case is ASDE ASDE L62: a 1"0=D ;1"0=L 1"0=+D;L, 1"0= s-euiv 9e can no( determine the euivalent total load allo(ed by ASD by usin! the desi!n ineuality: s-euiv 8 n/Ω s-euiv 8 n/1">? 0">0 n
!s"equiv # !n $ %%
LRFD
#he controllin! controllin! LRFD load combination euation euation in this case is LRFDE LRFDE L62: u 1"2D ;1">L 9e mae the )ollo(in! denitions: D +G,s-euiv L +1EG,s-euiv 9here is the percenta!e o) s-euiv that is dead dead load" Substitutin! these denitions into the load combination euation you !et: u 1"2+, s-euiv;1">+1E,s-euiv 1"> E 0"4Bs-euiv
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Similar .composite load )actors. can be developed )or other load combination euations" Substitutin! the above epression epression into the LRFD version o) the desi!n ineuality- (e !et u 8 φn 1"> E 0"4B s-euiv 8 φn s-euiv 8 φn / 1"> E 0"4B s-euiv 8 0"@0 n / 1"> E 0"4B
!s"equiv # !n $ %'% # * %+,-
6omparison 9e can no( compare the results by !raphin! the resultin! euations )or s-euiv/ n" Fi!ure 2"5"1 sho(s the compared load limits based on percenta!e dead load" From Fi!ure 2"5"1 you can see that- )or this case- (henever the total service load is 2
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%ote that the use o) other load combination euations (ill yield dierent results"
Figure ./ Comparison of LRFD & ASD Results