Overview of Flow Oscillations in Transonic and Supersonic Nozzles

[1]  W. G. Hill,et al.  Increased Turbulent Jet Mixing Rates Obtained by Self-Excited Acoustic Oscillations , 1977 .

[2]  T. C. Adamson,et al.  Analysis of unsteady transonic channel flow with shock waves , 1975 .

[3]  L. Cambier,et al.  elsA - An efficient object-oriented solution to CFD complexity , 2002 .

[4]  Sébastien Deck,et al.  Numerical Simulations of Steady and Unsteady Separated Nozzle Flows , 2002 .

[5]  F. Culick.  Oscillatory and unsteady processes in liquid rocket engines , 1993 .

[6]  Anjaneyulu Krothapalli,et al.  Discrete tones generated by a supersonic jet ejector , 1996 .

[7]  The response of normal shocks in diffusers , 1985 .

[8]  Ching Y. Loh,et al.  Numerical Investigation of Transonic Resonance with a Convergent-Divergent Nozzle , 2002 .

[9]  A. Jameson.  Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings , 1991 .

[10]  T. Bogar,et al.  Characteristic frequencies of transonic diffuser flow oscillations , 1983 .

[11]  T. Bogar,et al.  Characteristic frequency and length scales in transonic diffuser flow oscillations , 1981 .

[12]  T. Coakley,et al.  Downstream boundary effects on the frequency of self-excited oscillations in transonic diffuser flows , 1987 .

[13]  S. Verma,et al.  Unsteady Nature of Flow Separation Inside a Thrust Optimized Parabolic Nozzle , 2003 .

[14]  K. Matsuo,et al.  Mechanism of Shock Wave Oscillation in Transonic Diffusers , 2003 .

[15]  G. Meier,et al.  Oscillation modes of laval nozzle flow , 1995 .

[16]  T. C. Adamson,et al.  Large Amplitude Shock-Wave Motion in Two-Dimensional, Transonic Channel Flows , 1978 .

[17]  G. Dumnov,et al.  Unsteady side-loads acting on the nozzle with developed separation zone , 1996 .

[18]  Craig A. Hunter,et al.  Experimental Investigation of Separated Nozzle Flows , 2004 .

[19]  J. C. Kroutil,et al.  Shock-Wave Oscillations in a Transonic Diffuser Flow , 1979 .

[20]  A. Hussain,et al.  The ‘whistler-nozzle’ phenomenon , 1982, Journal of Fluid Mechanics.

[21]  G. Casalis,et al.  Shock Oscillations in Diffuser Modeled by a Selective Noise Amplification , 1999 .

[22]  J. F. Wasserbauer,et al.  Experimental and analytical investigation of the dynamic response of a supersonic mixed-compression inlet , 1968 .

[23]  M. Sajben,et al.  Effects of Initial Boundary-Layer Thickness on Transonic Diffuser Flows , 1981 .

[24]  Ganesh Raman,et al.  ADVANCES IN UNDERSTANDING SUPERSONIC JET SCREECH: REVIEW AND PERSPECTIVE , 1998 .

[25]  F. Culick,et al.  The response of normal shocks in diffusers , 1981 .

[26]  H. Wong,et al.  Theoretical prediction of resonance in nozzle flows , 2005 .

[27]  Sébastien Deck,et al.  Numerical simulation of side loads in an ideal truncated nozzle , 2002 .

[28]  Gerald Hagemann,et al.  Restricted Shock Separation in Rocket Nozzles , 2000 .

[29]  H. C. Yee.  Upwind and Symmetric Shock-Capturing Schemes , 1987 .

[30]  Khairul Q. Zaman,et al.  Investigation of a ‘transonic resonance’ with convergent–divergent nozzles , 2002, Journal of Fluid Mechanics.

[31]  T. Coakley,et al.  Numerical simulations of unsteady transonic flow in diffusers , 1982 .

[32]  A. Kistler,et al.  Fluctuating wall pressure under a separated supersonic flow , 1964 .