Development and validation of a 3D linearized Euler solver

Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference

Volumn 4, Issue , 2006, Pages 2336-2360

  Lan, Justin H ^a,b,c   Breard, Cyrille ^a  

^a BOEING COMPANY   (United States)

^b Acoustics and Fluid Mechanics Technology

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

3D LINEARIZED EULER SOLVER; INFLOW CONTROL DEVICE (ICD); NACELLE DROOP; NON-UNIFORM MEAN FLOW;

ACOUSTIC IMPEDANCE; AIRCRAFT; ANECHOIC CHAMBERS; ANTENNA PHASED ARRAYS; BOUNDARY CONDITIONS; CONVERGENCE OF NUMERICAL METHODS; FREQUENCY DOMAIN ANALYSIS; MATHEMATICAL MODELS; MICROPHONES; TURBOFAN ENGINES; VORTEX FLOW;

ACOUSTIC WAVE PROPAGATION;

EID: 33845614418     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Lan, J. H., Guo, Y., and Breard, C., "Validation and Application of Two Frequency Domain Acoustic Propagation Codes," AIAA 2003-3244.
2. Lan, J. H., Guo, Y., and Breard, C., "Validation of Acoustic Propagation Code with JT15D Static and Flight Test Data," AIAA 2004-2986.
3. Lan, J. H., and Breard, C., "Validation of 3D Acoustic Propagation Code with analytical and Experimental Results," AIAA 2005-2901.
4. Tam, C. K. W., Webb, J. C., "Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics," J. Comp. Phys. 107, 1993, pp. 262-281.
5. Gaitonde, D. V., and Visbal, M. R., "Further Development of Navier-Stokes Solution Procedure Based On Higher-Order Formulas," AIAA 99-0557.
6. Farassat, F., and Dunn, M. H., "A Simple Derivation of the Acoustic Boundary Condition in the Presence of Flow," J. Sound and Vibration, 224(2), July 8, 1999, pp. 384-386.
7. Jones, M.G., Watson, W.R., and Parrott, T.L., "Benchmark Data for Evaluation of Aeroacoustic Propagation Codes with Grazing Flow," AIAA 2005-2853.
8. Jones, M.G., Watson, W.R., and Parrott, T.L., "Benchmark Data for Evaluation of Aeroacoustic Propagation Codes with Grazing Flow," AIAA 2005-2853 Spreadsheet Database.
9. Sutliff, D.L., Heidelberg, L.J., Elliott, D.M., and Nallasamy, M., " Baseline Acoustic Levels of the NASA Active Noise Control Fan Rig," AIAA 96-1745.
10. Bailly, C., Bogey, C., and Juve, D., "Computation of Flow Noise Using Source Terms in Linearized Euler's Equations," AIAA 2000-2047.
11. Fuller, C.R., "Free-Field Correction Factor for Spherical Acoustic Waves Impinging on Cylinders," AIAA 87-2735.
12. Lan, J.H., Premo, J.W., and Sutliff, D.L., "Inlet Mode Measurements with an Inflow Control Device Microphone Array," AIAA 2002-2563.
13. Castres, F., Joseph, P., and Astley, J., "Mode Detection in Turbofan Inlets from Acoustic Pressure Measurements in the Radiated Field," AIAA 2004-2953.