Everyone,
This will become obvious below but we must distinguish between FEM analysis and software that produces reinforcement/prestress requirements based on FEM analysis. All FEM produces is a set of stresses which, when convereted to moments, describe the moments on the floor system that have to be designed for.
A tacked on design program then designs reinforcement. FEM does not produce reinforcement drawings, someones interpretation of FEM results does, whether it be done manually or by computer.
1 FEM vs EFM: There is no difference in the overall moment over a panel width between the 2. This can be easily verfied by setting up a simple square grid of columns in FEM and the same EFM sample and comparing the results. The whole thing should add up to wL^2/8 in each direction (same as for EFM) for a uniform load. If it does not, change FEM programs because the one you are using is WRONG.
The difference is that FEM tells us the distribution of thre moments across the slab based on elastic analysis while with EFM we have to guess the distribution based on experience, eg 75/25 for maximum negative moment and 60/40 or 55/45 for maximum positive moments and varying between.
Both methods should give the same total area of reinforcement over the width of a panel. There is no saving using FEM.
If software tells you there is a difference, question it because it is wrong. For example, if an FEM program allows for Mxy moments in the analysis and then ignores them in design (as several prominant ones do), then the difference will be at least 15% and possibly up to 25% UNDER estimation of the reinforcement requirements. This does not mean that you can use 15-25% less reinforcement, it means it has underdesigned by 15-25%.
It does not mean that FEM is wrong. FEM is reporting Mx, My and Mxy. It means that the design application tacked onto the end of the FEM is wrong because the developer does not understand design using FEM, or they are trying to cheat (hopefully it is the first but either is worrying).
2 I have no problem with EFM. It is how I design most times. What I do have a problem with is the assumption that the design moment on a PT flat slab is a total moment spread over the total width of a panel.
In RC design, ACI tells us to distribute the moments between column and middle strips in different propertions depending on whether it is at support or mid span. This fairly closely models the results of an FEM distribution of moments and I agree entirely with it.
In PT design ACI tells us to use the total moment over the total panel width (resulting in an average moment and averaged stresses over the entire width of the panel). This is blatently incorrect.
2--1 As I explained in earlier posts, for flat slabs where the tendons and reinforcement are placed in a pattern that provides a load path to the supports, it is possible to do the ultimate strength calculation the ACI way and work out a total capacity over the width of a panel rather than dividing into column and middle strips. The justification of this comes back to a yield line solution and the slab will stand up.
The 2 generally accepted tendon patterns for this are
1 a column/middle strip pattern in each direction with about 70% of the tendons in the coilumn strip and 30% in the middle strip in each direction - result is similar to the FEM moment result and the elastic response of the slab
2 a banded/distributed pattern with tendons equally spaced in one direction and concentrated over the columns in the other direction - result is a one way failure pattern completely different to the FEM moment result and to the elastic response of the slab
3 a third solution is similar to 1 but the ratios in each direction are varied but still consistent with each other. In this scenario, solution 2 is one extreme of the solutions possible.
In all cases, all of the laod is carried in each direction and there is a load path to the supports in the reinforcement pattern.
This yield line solution is only possible however when tendon layouts as described above are used, loads are uniform, concrete cross-section is uniform and the slab is uncracked at service - see below.
Otherwise solution 1 must be used where the tendon layout matches the elastic moment response of the slab.
2--2 The real problem with the ACI method arises when we come to serviceability design, crack control and deflections.
Concrete cracks based on the stresses at each point in the section, not based on the average stress over a 10m (33') width of slab. A Crack in concrete can only be restrained by reinforcement that crosses the crack. Sounds logical and obvious. But that is not the way ACI works for PT slabs.
The slab cracks based on the elastic moment pattern, not some assumed ultimate failure criterion. It keeps cracking as load is increased until the final ultimate capacity of the slab matches the reinforcement pattern. If that pattern is banded/distributed, then a lot of cracking and redistribution and extra deflection have to occur to achieve the final ultimate capacity.
What we are interested in is the first cracking and that is dependent on the elastic moments and their distribution across the floor panel. ACI ignores this.
Even though 75% of the moment is in only half of the width at the supports, ACI allows you to assume it is spread evenly. This means that you are grossly underestimating the actual stress which will crack the concrete. So ACI designers are assuming slabs are uncracked for cracking and deflection calculations when they are actually cracked. This is very unconservative. Add in the fact that everyone ignores restraing stresses and your software might be ignoring Mxy (15% of the moemnts) and your slabs will be a lot more cracked than you expect and deflections will be much higher.
The further serviceability problem is that banded/distributed slabs cannot be allowed to crack at service unless crack control reinforcememt, calculated based on the requiremnents of all areas of the slab for their actual stresses, is supplied based on the elastic moment pattern not the failure pattern. The decision on this cracking must be based on the elastic stress pattern and allow for restraing stresses due to shrinkage and temperature change.