The paper presents a new empirical model for the calculation of the er
ror shift of a turbine gas meter caused by disturbed velocity profiles
in front of the gas meter. The model is based on an extensive catalog
ue of fluid velocity profiles for different flow rates, perturbations
(bends, diffusors, half plates, double bends out of plane) and distanc
es between perturbation and turbine gas meter measured by a computer-c
ontrolled laser Doppler velocimeter system. The flow profiles can be c
haracterized by defining flow field parameters: the momentum-fluxes de
scribing the two-dimensional distribution of the axial and tangential
velocity component and the asymmetry of the flow characterized by an a
symmetry number. These parameters quantify the influence of flow pertu
rbations, swirl and deformation of the flow profile, and allow, in add
ition, the error shift to be calculated analytically using a simple mo
del based on only three flow field parameters. The developed model and
the catalogue of flow profiles thus allow the error shift to be predi
cted for many applications significant in practice, which is important
for the practical use of gas meters.