Modeling and control for axial flow compression systems have received great attention in recent years. The objectives are to suppress rotating stall and surge, to extend the stable operating range of the compressor system, and to enlarge domains of attraction of stable equilibria using feedback control methods. The success of this research field will significantly improve compressor performance and thus future aeroengine performance. This paper surveys the research literature and summarizes the major developments in this active research field, focusing on the modeling and control perspectives to rotating stall and surge for axial flow compressors. © 1999 IEEE
Rotating stall and surge are the two primary constraints for the performance of axial flow compresso...
March 1992Includes bibliographical references (p. 231-233)An active control system has been implemen...
The paper presents an analysis of the current state of the art in the control of aero- or hydrodynam...
Modeling and control for axial flow compression systems have received great attention in recent year...
Stable operation of both axial and radial compressors is constrained by rotating stall and surge. De...
Rotating stall is a primary constraint for the performance of axial flow compressors. This paper est...
Surge control is investigated in conjunction with rotating stall control for axial flow compressors ...
Classical bifurcation analysis for nonlinear dynamics is used to derive a nonlinear feedback control...
The useful range of operation in axial flow compressors is limited by aerodynamic flow instabilities...
Rotating stall is a fundamental aerodynamic instability in axial flow compressors, induced by nonlin...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993....
The objective of the work described in this thesis is twofold; to elucidate the nature of stall and...
General methodologies are proposed in this two-part paper that further phenomeno-logical understandi...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.I...
The paper presents an analysis of the current state of the art in the control of aero- or hydrodynam...
Rotating stall and surge are the two primary constraints for the performance of axial flow compresso...
March 1992Includes bibliographical references (p. 231-233)An active control system has been implemen...
The paper presents an analysis of the current state of the art in the control of aero- or hydrodynam...
Modeling and control for axial flow compression systems have received great attention in recent year...
Stable operation of both axial and radial compressors is constrained by rotating stall and surge. De...
Rotating stall is a primary constraint for the performance of axial flow compressors. This paper est...
Surge control is investigated in conjunction with rotating stall control for axial flow compressors ...
Classical bifurcation analysis for nonlinear dynamics is used to derive a nonlinear feedback control...
The useful range of operation in axial flow compressors is limited by aerodynamic flow instabilities...
Rotating stall is a fundamental aerodynamic instability in axial flow compressors, induced by nonlin...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993....
The objective of the work described in this thesis is twofold; to elucidate the nature of stall and...
General methodologies are proposed in this two-part paper that further phenomeno-logical understandi...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.I...
The paper presents an analysis of the current state of the art in the control of aero- or hydrodynam...
Rotating stall and surge are the two primary constraints for the performance of axial flow compresso...
March 1992Includes bibliographical references (p. 231-233)An active control system has been implemen...
The paper presents an analysis of the current state of the art in the control of aero- or hydrodynam...