Upasena
Structural
- Sep 26, 2008
- 11
Dear Sirs,
I am working on the design of an incrementally launched box girder bridge whose parameters are as follows:
2Nos. End spans 26.5 m each.
4 Nos. Internal Spans 46.5 m each.
All bearings are laminated elastomeric after launching. During the launching Teflon bearings are used to minimize the friction.
Cross section area of the box girder is 9.27 sq.m.
Width of the bridge deck 11 m.
Height of the box girder 3.2 m, yt=1.395 m, yb=1.805 m.
Moment of inertia of the box girder=13.06 m^4.
Post tension straight tendons 32 near supports each having 143 sq.mm csa.
CG of tendons are located 320 mm above the CG of the box girder.
Post tension straight tendons 28 in spans each having 143 sq.mm csa.
CG of tendons is located 258 mm below the CG of the box girder.
The bride is launched with a nose in front and on Teflon bearings, 10 m sections.
The bridge is designed for HB30 and HA loadings as per BS 5400.
I am new to the ILM bridge design. Proper analyses were carried out with Midas and Staad-pro
As our bridge cross section suffers no tension at any stage.
My question is: Have got to check the stresses for the ultimate shear resistance of a section cracked in flexure, Vcr. If so why? Are cracks likely form from thermal and creep effects?. I shall thank you to enlighten me on this crack stresses check. Is it usual to assume a cracked section?
K. W. Upasena
I am working on the design of an incrementally launched box girder bridge whose parameters are as follows:
2Nos. End spans 26.5 m each.
4 Nos. Internal Spans 46.5 m each.
All bearings are laminated elastomeric after launching. During the launching Teflon bearings are used to minimize the friction.
Cross section area of the box girder is 9.27 sq.m.
Width of the bridge deck 11 m.
Height of the box girder 3.2 m, yt=1.395 m, yb=1.805 m.
Moment of inertia of the box girder=13.06 m^4.
Post tension straight tendons 32 near supports each having 143 sq.mm csa.
CG of tendons are located 320 mm above the CG of the box girder.
Post tension straight tendons 28 in spans each having 143 sq.mm csa.
CG of tendons is located 258 mm below the CG of the box girder.
The bride is launched with a nose in front and on Teflon bearings, 10 m sections.
The bridge is designed for HB30 and HA loadings as per BS 5400.
I am new to the ILM bridge design. Proper analyses were carried out with Midas and Staad-pro
As our bridge cross section suffers no tension at any stage.
My question is: Have got to check the stresses for the ultimate shear resistance of a section cracked in flexure, Vcr. If so why? Are cracks likely form from thermal and creep effects?. I shall thank you to enlighten me on this crack stresses check. Is it usual to assume a cracked section?
K. W. Upasena