Current provisions of the ACI 318 Code and AASHTO Design Specification limi
t the nominal yield stress of spiral reinforcement for compression members
to 414 Wa (60 ksi). A procedure for the design of high-strength spiral rein
forcement for compression members is proposed and evaluated. The proposed m
ethod utilizes usable stress values, rather than nominal yield stress value
s, for spiral design. The research included large-scale axial load tests on
14 spirally reinforced concrete compression members with spiral reinforcem
ent yield stress values ranging from 538 to 1345 Wa (78 to 195 ksi) and usa
ble stress values ranging from 545 to 1131 Wa (79 to 164 ksi). It was found
that, for the compression member geometries and material properties treate
d in this study, the proposed design procedure satisfactorily predicted the
behavior of the compression members made from spirals with usable stress v
alues up to 758 Wa (110 ksi).