Meshes are commonly used as part of instruments for in situ atmospheric mea
surements. This study analyses the aerodynamic effect of meshes by means of
wind tunnel experiments and numerical simulations. Based on the Direct Sim
ulation Monte Carlo method, a simple mesh parameterisation is described and
applied to a number of representative flow conditions. For open meshes fre
ely exposed to the flow, substantial compression effects are found both ups
tream and downstream of the mesh. Meshes attached to close instrument struc
tures, on the other hand, cause only minor how disturbances. In an accompan
ying paper, the approach developed here is applied to the quantitative anal
ysis of rocket-borne density measurements in the middle atmosphere.