MODELING FOR CONTROL OF ROTATING STALL

An analytical model for control of rotating stall has been obtained fr om the basic fluid equations describing the process at inception. The model describes rotating stall as a traveling wave packet, sensed-in s patial components-via the Fourier decomposition of measurements obtain ed from a circumferential array of evenly distributed sensors (hot wir es) upstream of the compressor. A set of ''wiggly'' inlet guide vanes (IGVs) equally spaced around the compressor annulus constitute the ''f orced'' part of the model. Control is effected by launching waves at a ppropriate magnitude and phase, synthesized by spatial Fourier synthes is from individual IGV deflections. The effect of the IGV motion on th e unsteady fluid process was quantified via identification experiments carried out on a low speed, single-stage axial research compressor. T hese experiments served to validate the theoretical model and refine k ey parameters in it. Further validation of the model was provided by t he successful implementation of a complex-valued proportional control law, using a combination of first and second harmonic feedback; this r esulted in an 18% reduction of stalling mass flow, at essentially the same pressure rise.