Highlights of aeroacoustics research in the U.S. - 1998

Journal of Sound and Vibration

Volumn 228, Issue 3, 1999, Pages 589-610

  Raman, G ^a   Mclaughlin, D K ^b  

^a Illinois Institute of Technology   (United States)

^b The Pennsylvania State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0039842877     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1999.2429     Document Type: Article

References (23)

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2. E. ENVIA, D. L. HUFF and C. R. MORRISON 1996 American Institute of Aeronautics and Astronautics Paper 96-1791. Analytical assessment of stator sweep and lean in reducing rotor-stator tone noise.
3. E. ENVIA and M. NALLASAMY 1998 NASA TM-1998-208662. Design selection and analysis of a swept and leaned stator concept.
4. F. FARASSAT and K. S. BRENTNER 1998 Journal of Sound and Vibration 218, 481-500. Supersonic Quadrupole noise theory for high-speed helicopter rotors.
5. F. FARASSAT, K. S. BRENTNER and M. H. DUNN 1998 American Institute of Aeronautics and Astronautics Paper 98-2375. A study of supersonic surface sources - the Ffowcs Williams-Hawkings equation and the Kirchhoff formula.
6. K. K. AHUJA and R. J. GAETA, Jr. 1997 American Institute of Aeronautics and Astronautics Paper 97-1701. A new wide-band acoustic liner with high temperature capability.
7. R. J. GAETA, Jr. and K. K. AHUJA 1997 American Institute of Aeronautics and Astronautics Paper 97-1700. A unique flow-duct facility to measure liner performance in cold and heated flows.
8. T. A. MANNING and S. K. LELE 1998 American Institute of Aeronautics and Astronautics Paper 98-0282. Numerical simulations of shock-vortex interactions in supersonic jet screech.
9. H. SHEN and C. K. W. TAM 1998 American Institute of Aeronautics and Astronautics Journal 36, 1801-1807. Numerical simulation of the generation of axisymmetric mode jet screech tones.
10. J. FREUND, S. LELE and P. MOIN 1998 American Institute of Aeronautics and Astronautics Paper 98-2291. Direct numerical simulation of a Mach 1-92 turbulent jet and its sound field.
11. J. L. STROMBERG, D. K. MCLAUGHLIN and T. R. TROUTT 1980 Journal of Sound and Vibration 72, 159-176. Flow field and acoustic properties of a Mach number 0·9 jet at low Reynolds number.
12. R. HIXON, S. H. SHIH and R. R. MANKBADI 1997 NASA CR-202338 (ICOMP-97-04). Numerical simulation of the effect of heating on supersonic jet noise.
13. P. J. MORRIS, L. N. LONG, A. BANGALORE and Q. WANG 1997 Journal of Computational Physics 133, 56-74. A parallel three-dimensional computational aeroacoustics method using nonlinear disturbance equations.
14. P. J. MORRIS, L. N. LONG, Q. WANG, T. SCHEIDEGGER and A. R. PILON 1998 AIAA/CEAS Paper 98-2290. High speed jet noise simulations.
15. R. HIXON, S. H. SHIH, R. R. MANKBADI and J. R. SCOTT, J. R. 1998 American Institute of Aeronautics and Astronautics Paper 98-3241. Time-domain solution of the airfoil gust problem using a high-order compact scheme.
16. S. H. SHIH, R. HIXON, L. A. POVINELLI and R. R. MANKBADI 1998 American Institute of Aeronautics and Astronautics Paper 98-3014. Large-scale simulation of supersonic jet noise.
17. S. H. SHIH, R. HIXON, R. R. MANKBADI, A. PILON and A. LYRINTZIS 1997 American Institute of Aeronautics and Astronautics Paper 97-0282. Evaluation of far-field jet noise prediction methods.
18. Y. OZYORUK, L. N. LONG and M. G. JONES 1998 Journal of Computational Physics 146, 29-57. Time-domain numerical simulation of a flow-impedance tube.
19. J. LIU and L. N. LONG 1998 American Institute of Aeronautics and Astronautics Paper 98-2330. Direct aeroacoustic and aerodynamic simulation of multi-hole engine liners.
20. T. CHYCZEWSKI, L. N. LONG and P. J. MORRIS 1998 American Institute of Aeronautics and Astronautics Journal 36, 986-993. Numerical study of nozzle exit condition effects on jet development.
21. L. N. LONG, P. J. MORRIS, K. MOROONEY and S. KELLOGG 1998 Journal of Engineering Education 87. The teaching and learning of high performance computing.
22. J. M. SEINER 1998 Theoretical and Computational Fluid Dynamics 10, 373-383. A new rational approach to jet noise reduction.
23. Aeronautics and Space Transportation Technology, Three Pillars for Success. NASA Annual Progress Report 1997-1998. Publication of the NASA Office of Aeronautics and Space Transportation Technology, Code R, NASA HQ, NP-1998-10-242-HQ.