The dynamic stability behavior of a typical pilot-operated relief valv
e has been investigated both numerically and experimentally. The valve
piston equation of motion has been solved in connection with the cons
ervation equations of the oscillating flow in the attached riser. The
boundary condition at the riser tip is of a choked flow type and had t
o be given special attention in oscillatory flows. Pertinent quasi-ste
ady flow equations have been formulated to describe the different phas
es of relief along the piston lift. A model describing the process of
pressure relief is described briefly, followed by a parametric study o
f the effects of various factors on the oscillation levels and charact
ers. Field measurements were taken on an NPS 8 pilot-operated dual-out
let relief valve mounted on a riser assembly of L/D = 15 in a natural
gas compressor station.