PSE applied to supersonic jet instability

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Malik, M R ^a   Chang, C L ^a  

^a High Technology Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; AEROSPACE ENGINEERING; NONLINEAR EQUATIONS; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS;

AXISYMMETRIC MODES; DISTURBANCE GROWTH; INSTABILITY MODES; LOW REYNOLDS NUMBER; NONLINEAR EFFECT; NONLINEAR EVOLUTIONS; PARABOLIZED STABILITY EQUATIONS; SUPERSONIC JETS;

FIGHTER AIRCRAFT;

EID: 84983146187     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (32)

1. Balakumar, P. and Malik, M. R., "Supersonic Jet Noise Prediction and Control," HTC Final Report NAS3-27205, 1994.
2. Bangalore, A., Morris, P. J., and Long, L. N., 1996 "A Parallel Three-Dimensional Computational Aeroacoustics Methods Using Non-Linear Disturbance Equations," AIAA 96-1728.
3. Bertolotti, F. P., 1991 "Compressible Boundary Layer Stability Analyzed with the PSE Equations," AIAA 91-1637.
4. Bertolotti, F. P., Herbert, Th. and Spalart, P. R., 1992 "Linear and Nonlinear Stability of the Blasius Boundary Layer," J. Fluid Mech. 242, pp. 441-474.
5. Brown, G. L. and Roshko, A., 1974 "On Density Effects and Large Structure in Turbulent Mixing Layers," J. Fluid Mech. 64(4), pp. 775-816.
6. Chang, C.-L. and Malik, M. R., 1994 "Oblique-Mode Breakdown and Secondary Instability in Supersonic Boundary Layers," J. Fluid Mech. 273, pp. 323-359.
7. Chang, C.-L., Malik, M. R., Erlebacher, G. and Hussaini, M. Y., 1991 "Compressible Stability of Growing Boundary Layers Using Parabolized Stability Equations," AIAA 91-1636.
8. Crow, S. C. and Champagne, F. H., 1971 "Orderly Structure in Jet Turbulence," J. Fluid Mech. 48(3), pp. 547-591.
9. Goldstein, M. E. and Choi, S.-W., 1989 "Nonlinear Evolution of Interacting Oblique Waves in Two-Dimensional Shear Layers," J. Fluid Mech. 207, pp. 97-120.
10. Herbert, Th., 1991 "Boundary-Layer Transition -Analysis and Prediction Revisited," AIAA 91-0737.
11. Joslin, R. D., Streett, C. L., and Chang, C.-L., 1992 "3-D Incompressible Spatial Direct Numerical Simulation Code Validation Study-A Comparison with Linear Stability & Parabolic Stability Equation Theories for Boundary-Layer Transition on a Flat Plate," NASA TP-3205.
12. Lepicovsky, J., Ahuja, K. K., Brown, W. H., and Burrin, R. H. 1985 "Coherent Large-Scale Structures in High Reynolds Number Supersonic Jets," NASA CR-3952.
13. Li, F. and Malik, M. R., 1994 "Mathematical Nature of Parabolized Stability Equations," Proc. of IUTAM Symp. on Laminar-Turbulent Transition, Sendai, Japan, (Ed. R. Kobayashi), Springer, pp. 205-212.
14. Malik, M. R., Chuang, S., and Hussaini, M. Y., 1982 "Accurate Numerical Solution of Compressible Stability Equations," ZAMP 33, pp. 189-201.
15. Malik, M. R., Li, F., and Chang, C.-L., 1994 "Crossflow Disturbances in Three-Dimensional Boundary Layers: Nonlinear Development, Wave Interaction and Secondary Instability," JFM 268, pp. 1-36.
16. Mankbadi, R. R., Mayer, M. E., and Povinelli, L. A., 1994 "Structure of Supersonic Jet Plow and its Radiated Sound," AIAA J. 32(5).
17. McLaughlin, D. K, Morrison, G. L., and Troutt, T. R., 1977 "Reynolds Number Dependence in Supersonic Jet Noise," AIAA J. 15, pp. 526-532.
18. McLaughlin, D. K., Morrison, G. L., and Troutt, T. R., 1975 "Experiments on the Instability Waves in a Supersonic Jet and Their Acoustic Radiation," J. Fluid Mech., 69, pp. 73-95.
19. Morris, P. J. and Tarn, C. K. W., 1977 "Near and Far Field Noise for Large-Scale Instabilities of Axisymmetric Jets," AIAA 77-1351.
20. Morrison, G. L. and McLaughlin, D. K., 1980 "Instability Process in Low Reynolds Number Supersonic Jets," AIAA J. 18(7), pp. 793-800.
21. Morrison, G. L. and McLaughlin, D. K., 1979 "The Noise Generated by Instabilities in Low Reynolds Number Supersonic Jets," J. Sound & Vibration, 65(2), pp. 177-191.
22. Seiner, J. M., Bhat, T. R. S., and Ponton, M. K., 1993 "Mach Wave Emission from a High Temperature Supersonic Jet," AIAA 93-0734.
23. Spall, R. E. and Malik, M. R., 1989 "Goertler Vortices in Supersonic and Hypersonic Boundary Layers," Phys. Fluids A 1(11), pp. 1822-1835.
24. Stromberg, J. L., McLaughlin, D. K., and Troutt, T. R., 1979 "Flowfield and Acoustic Properties of a Mach number 0.9 Jet at a Low Reynolds Number," AIAA 79-0593.
25. Tarn, C.K.W., 1971 "Directional Acoustic Radiation from a Supersonic Jet Generated by Shear Layer Instability," J. Fluid Mech.46, pp. 757-768.
26. Tarn, C. K. W., 1972 "On the Noise of a Nearly Ideally Expanded Supersonic Jet," J. Fluid Mech. 51, pp. 69-95.
27. Tarn, C. K. W., 1991 "Jet Noise Generated by Large-Scale Coherent Motion," in Aeroacoustics of Flight Vehicles: Theory and Practice, Vol. 1: Noise Sources, NASARP-1258, WRDC TR-90-3052.
28. Tarn, C. K. W. and Burton, D. E., 1984 "Sound Generated by Instability Waves of Supersonic Flows. Part 2. Axisymmetric Jets," J. Fluid Mech., 138, pp. 273-295.
29. Tarn, C. K. W., Chen, P., and Seiner, J. M., 1991 "Relationship Between Instability Waves and Noise of High-Speed Jets," AIAA 91-0492.
30. Thompson, K. W., 1987 "Time Dependent Boundary Conditions for Hyperbolic Systems," J. Comput. Phys. 68, pp. 1-24.
31. Troutt, T. R. and McLaughlin, D. K., 1982 "Experiments on the Flow and Acoustic Properties of a Moderate-Reynolds-Number Supersonic Jet," J. Fluid Mech. 116, pp. 123-156.
32. Viswanathan, K. and Sankar, L. N., 1995 "Toward the Direct Calculation of Noise: Fluid/Acoustic Coupled Approach," AIAA J. 33(12), pp. 2271-2279.