Moment Release in STAAD Pro:
In the given illustration a bay frame with 5 m length, 5 m width & 3 m height is considered & between two primary beams (beams which are supported directly over columns) on secondary beam (beam supported over primary beam) is provided.
The secondary beam is loaded with 20 Kn/m UDL, no other weight is considered on any other members.

Fig.1 Bay frame with Loading & beam numbers

Case-1:
when the secondary beam is fixed at joints at primary beam & no release command is given.

Bending Moment:
If you notice in the below given figure-2 you can see that hogging moments are coming on the top face of the secondary beam near the joints, this is because when this beam under loading tries to undergo bending in downward direction the rigidity of the joint at secondary & primary beam junction restrains it & thus because of this restraining action hogging moments arise on the top face of the secondary beam.

Fig.2 Bending Moment Diagram

Torsion:
Moreover due to rigidity at joint the secondary beam also tries to rotate the primary beams about their own axis in inward direction which will result in arise of torsional moments in the primary member (refer figure-3). Upon analysis in the given condition the joints are treated as rigid offering restraints to all three force directions (Fx, Fy & Fz) & all three moment directions (Mx, My & Mz) & thus torsion or twisting moment about the local axis of primary beams is generated. In the given case 11.51 Knm torsional moment is coming in primary members.

Fig. 3 Torsional Moments in Primary Members when supported secondary beam is not released

Fig. 4 Torsional moments coming in primary members in un-released condition

Case-2:
When secondary beam is released at joints & is assumed to be simply supported over the primary beams.
In this case secondary beam has been provided with member release command & bending moment about Z i.e. MZ moment is released (you can notice two tiny circles near joints denoting member release command), in our case we have considered 100% release.

Bending Moment:
When a member is released at a joint then STAAD will not consider that joint as a rigid joint/node offering restraints in all three force directions (Fx, Fy & Fz) & all three moment directions (Mx, My & Mz) & instead it will release the force or moment restraint as defined in member release command. In this case as we said above we have given member release in Mz, so all the bending moment in Mz is free (without restraint) & due to this the behaivour of the beams has changed & because of that only sagging moments (as in the case of simply supported member) are coming on the bottom face of the beam & no hogging moments will come (refer figure-5).

Fig. 5 Bending moment when secondary beam is released


Torsion:
Now as the condition of the joint is simply supported & with no restraint offered by primary beams to the secondary beam in bending the secondary beam undergoes bending freely & thus no torsion or twisting of primary members happen, that means zero torsion in primary members.


Fig. 6 Zero torsion in primary members supporting secondary beam with member release command




Conclusion: Below given is the comparative analysis of the above two cases;

S.no.
Point Observed
Joint conditions
Remarks
Without Member Release command
With member release command (100% release in Mz)
1.
Rigidity at the joint & support condition
Fixed Support condition.
STAAD Pro treats the Joint/node as rigid & thus upon analysis restraints is provided in all three force directions (Fx, Fy & Fz) & all three moment directions (Mx, My & Mz).
Simply Supported condition.
With release command the joint is released in the specified force or moment & thus no restraint is offered for the same, in our case Mz release is used.

2.
Hogging Moment in Secondary Beam at Top face near supports.
23.02 KNm
0.0 Knm
Reinforcement at top will be more in without member release command.
3.
Sagging moment at bottom mid face of the secondary beam.
-39.48 knm
-62.50 knm
Reinforcement at bottom face of the beam will be higher in member released case due to concentration of moments at bottom face.
4.
Torsion In primary beams.
11.51 Knm
0.0 knm
In without member release case the nos. of the stirrups or transverse reinforcement will be increased in primary beams i.e. stirrups will be required at closer spacing.
5.
Bending moment & shear force in primary beams.
Same
Same

1.  Generally, member release command is given in conventional design practice whenever the primary beam member fails because of torsional moments.
2.     Although it is conventional but it is always advised to make sure that the assumption of member release holds true as per the actual conditions of the structure.

3.   Member release shall be avoided because it causes reduction in nos. of stirrups of the primary member & which in turn reduces the ductility of the member, further the concrete & main reinforcement of beams with less no. of stirrups then required will not be confined properly. Poor ductility & poor confinement is not good for the structure for its resistance to seismic forces. 

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