Analysis of Inlet-Compressor Acoustic Interactions Using Coupled CFD Codes

A. Suresh and S.E. TownsendDynacs Engineering, Inc., Brook Park, OhioG.L. Cole, J.W. Slater, and R. ChimaLewis Research Center, Cleveland, OhioPrepared for the37th Aerospace Sciences Meeting and Exhibitsponsored by the American Institute forAeronautics and AstronauticsReno, Nevada, January 11-14, 1999National Aeronautics andSpace AdministrationLewis Research Center

[1]  A. Abdel-Fattah Education Committee Best Paper of 1996 Award: Response of a Turbofan Engine Compression System to Disturbed Inlet Conditions , 1997 .

[2]  Joongkee Chung,et al.  Comparison of compressor face boundary conditions for unsteady CFD simulations of supersonic inlets , 1995 .

[3]  Gerald Paynter Modeling the response from a cascade to an upstream convective velocity disturbance , 1998 .

[4]  Doug Garrard,et al.  A One Dimensional, Time Dependent Inlet / Engine Numerical Simulation for Aircraft Propulsion Systems , 1997 .

[5]  Miklos Sajben,et al.  Experimental investigation of outflow boundary conditions used in unsteady inlet flow computations , 1997 .

[6]  John W. Slater,et al.  STUDY OF CFD METHODS APPLIED TO RAPIDLY DEFORMING BOUNDARIES , 1997 .

[7]  John W. Slater,et al.  NPARC v3.1 User's Guide: A Companion to the NPARC v3.0 User's Guide , 1999 .

[8]  Miklos Sajben,et al.  Experimental exploration of compressor-face boundary conditions for unsteady inlet flow computations , 1995 .

[9]  P. Woodward,et al.  The numerical simulation of two-dimensional fluid flow with strong shocks , 1984 .

[10]  Jeffrey A. Lewis,et al.  Supersonic inlet simulation with closed-loop control of moving control surfaces , 1996 .

[11]  John W. Slater,et al.  Compressor-face boundary condition experiment - Generation of acoustic pulses in annular ducts , 1996 .

[12]  Miklos Sajben,et al.  Reflection of Large Amplitude Acoustic Pulses from an Axial Flow Compressor , 1997 .

[13]  G. Paynter,et al.  Prediction of supersonic inlet unstart caused by freestream disturbances , 1994 .

[14]  Gary L. Cole,et al.  Modeling the Response from a Cascade to an Upstream Acoustic Disturbance , 2000 .

[15]  Gary L. Cole,et al.  Computational Methods for HSCT-Inlet Controls/CFD Interdisciplinary Research , 1994 .

[16]  Keith Numbers,et al.  DEVELOPMENT OF A COUPLED INLET-ENGINE DYNAMIC ANALYSIS METHOD , 1997 .

[17]  Gerald C. Paynter,et al.  Response of a two-dimensional cascade to an upstream disturbance , 1997 .

[18]  Milt Davis,et al.  DYNamic Turbine Engine Compressor Code (DYNTECC) - Theory and capabilities , 1992 .