The role of the feedback phenomenon in many aeroacoustics problems of current interest

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Ahuja, K K ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; AEROSPACE ENGINEERING; FEEDBACK;

ACOUSTIC RESONANCE; CAVITY NOISE; INDUSTRIAL PROCESSS; INSTABILITY WAVES; SELECTED EXAMPLES; SHEAR LAYER; SOUND IMPINGING;

SHEAR FLOW;

EID: 85088719905     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-77     Document Type: Conference Paper

References (126)

1. Smith, Michael, J. T., "Aircraft Noise," Cambridge University Press, 1989.
2. Ingard, K. U., "Fundamentals of Waves and Oscillations," Cambridge University Press, 1988.
3. Tyndall, J., "On the Action of Sonorous Vibrations on Gaseous and Liquid Jets," Phil. Mag., Vol. 33, pp. 375-391, 1857.
4. Lepicovsky, J., Ahuja, K. K., Brown, W. H., Salikuddin, M. and Morris, P. J., "Acoustically Excited Heated Jets - Internal Excitation," NASA Final Report, NASA CR-4129, 1988.
5. Ahuja, K. K., Lepicovsky, J., Tarn, C. K. W., Morris, P. J., and Burrin, R. H., "Tone-Excited Jet: Theory and Experiments, Final Report, NASA CR-3538, 1982.
6. Ahuja, K. K., and Burrin, R. H., "Control of Flow Separation by Sound," AIAA 84-2298, 9th AIAA Aeroacoustics Conference, Williamsburg, VA, October 1984.
7. Ahuja, K. K. and Burrin, R. H., "Control of Flow Separation by Sound," AFWAL-TR-84-3096, 1984.
8. Elkoby, R., "Acoustic Excitation of Wing Wake Flows," Masters Thesis, Georgia Institute of Technology, December 2000.
9. Zaman, K. B. M. Q., "Effect of Acoustic Excitation on Stalled Flows over an Aerofoil," AIAA-90-4010, 1990. Also appeared as N AS ATM 103183(1990).
10. Brown, G. B., "The Vortex Motion Causing Edge Tones," Proc. Phys. Soc. (London), Vol 49, pp493-507, 1937
11. Curie, N., "The Mechanism of Edgetones," Proc. Roy. Soc. London, A216, 412, 1953.
12. Powell, A., "On the Edgetone," J. Acoust. Soc.Am, Vol. 33, pp. 95-409, 1961.
13. Powell, A., "On the Edgetone and Associated Phenomena" Acoustica, Vol. 3, pp. 281-284, 1963.
14. Coltman, J. W., "Jet Noise Drive Mechanisms in Edge Tones and Organ Pipes," J. Acoust. Soc.Am, Vol. 49, 752-733, 1976.
15. Lepicovsky, J., and Ahuja, K. K., "Experimental Results on Edge- Tone Oscillations in High-Speed Subsonic Jets," AIAA Journal, Vol. 23, No. 10, pp. 1463-1468, 1985.
16. Tarn, C. K. W. and Ahuja, K. K., "Theoretical Model of Discrete Tone Generation by Impinging Jets," Journal of Fluid Mechanics, Vol. 214, pp. 67-87, 1990.
17. Wagner, F. R., "The Sound and Flow field of an Axially Symmetric Free Jet Upon Impact on a Wall," NASA TT F-13942, 1971.
18. Neuwerth, G., "Acoustic Feedback of a Subsonic and Supersonic Free Jet which Impinges on an Obstacle," 5th DGLR Meeting, Berlin, 1972. ((1972).
19. Ahuja, K. K., Tarn, C. K. W., Salikuddin, M., Burrin, R. H., Roads, R. "Aeroacoustic Environment of Single and Twin Impinging Model Plumes in Relation to STOVL Aircraft. I - Experimental and Analytical Results," NASA CR-4291, VoL.1, 1990.
20. Ahuja, K. K., and Blakney, D. F., "Tone Excited Jets - Part IV: Acoustic Measurements," Journal of Sound and Vibration, Vol. 102(1), pp. 93-117, 1985.
21. Michalke, A, " A Survey on Jet Instability Theory,"Prog. Aerspace Sciences., Vol. 21, pp. 159-199, 1984.
22. Tam, C. K. W. and Burton, D. E., "Sound Generated by Instability Waves of Supersonic flow. Part 2: Axisymmetric Jets," Journal of Fluid Mechanics, Vol. 138, pp. 273-295,1984.
23. Ho, C. M and Nossier, N. S., "Dyynamics of an Impinging Jet, Part 1. The Feedback Phenomenon," J. Fluid Mech., Vol 105, pp. 119-142, 1981.
24. Neuwerth, G., "Acoustic Feedback of a Subsonic and Supersonic Free Jet which Impingeson an Obstacle," 5th DGLR Meeting, Berlin, 1972.by Neuwerth14 (1972).
25. Wagner, F. R., "The Sound and Flow field of an Axially Symmetric Free Jet Upon Impact on a Wall," NASA TT F-13942, 1971.
26. Ahuja, K. K., Tam, C. K. W., Salikuddin, M., Burrin, R. H., Roads, R. "Aeroacoustic Environment of Single and Twin Impinging Model Plumes in Relation to STOVL Aircraft. I - Experimental and Analytical Results," NASA CR-4291, Vol. 1, 1990
27. Ahuja, K. K., and Spencer, D. A., "Aeroacoustics of Advanced STOVL Aircraft Plumes," Proceedings of the International Powered Lift Conference and Exposition:P-203, Santa Clara, CA, December 7-10, 1987, Published by SAE; pp. 531-542, February 1988.
28. Ahuja, K. K. and Brown, W. H., "Shear Flow Control by Mechanical Tabs," A1AA 89-0994, 2nd AIAA Shear Flow Conference, Tempe, AZ, March 1989
29. Ahuja, K. K., Massey, K. C., and Entrekin, A. C, "Contribution of Mixing Within an Ejector to the Farfield Noise Measurements," AIAA Paper 96-0639, 34th AIAA Aerospace Sciences Meeting, Reno, Nevada, January 15-18, 1996.
30. Samimy, M., Zaman, K. B. M. Q., and Reeder, M. F., "Supersonic Jet Mixing Enhancement by Vortex Generators," AIAA Paper 91- 2263, June 1991
31. Brown, W. H., and Ahuja, K. K., "Jet and Wing/Flap Interaction Noise," AIAA 84-2362, 9th AIAA Aeroacoustics Conference, Williamsburg, VA, October 1984.
32. Ahuja, K. K., "Aeroacoustic Performance of Open-Jet Wind Tunnels with Particular Reference to Jet/Collector Interactions," Final Report AEDC-SBIR-94-02, June 1995.
33. Lepicovsky, J., and Ahuja, K. K., "Experimental Results on Edge- Tone Oscillations in High-Speed Subsonic Jets," AIAA Journal, Vol. 23, No. 10, pp. 1463-1468, 1985.
34. Ahuja, K. K., Massey, K. C., and D'Agostino, M. S., "Flow/Acoustic Interactions in Open-Jet Wind Tunnels," AIAA 97- 1691, 3rd Joint AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, May 12-14, 1997.
35. Ahuja, K. K., "Aeroacoustic Performance of Open-Jet Wind Tunnels with Particular Reference to Jet/Collector Interactions," Final Report AEDC-SBIR-94-02, June 1995.
36. Ahuja, K. K., Massey, K. C., and D'Agostino, M. S., "Flow/Acoustic Interactions in Open-Jet Wind Tunnels," AIAA 97- 1691, 3rd AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, May 12-14, 1997.
37. Shaw, Leonard, Clark, Rodney, and Talmadge, Dick, "F-l 1 Generic Weapons Bay Acoustics Environment," Journal of Aircraft, Vol. 14, No. 7, pp. 833-837, September 1977.
38. Karamcheti, K., "Acoustic Radiation from two-Dimensional Rectangular Cutouts in Aerodynamic Surfaces," NACA TN 3487, August 1955.
39. Heller, H. H., and Bliss, D. B., "Aerodynamically induced pressure oscillations in cavities - Physical mechanisms and suppression concepts," Tech. Rep. AFFDL_TR_74-133. AF Flight Dyn. Lab., Wright Patterson Air Force Base, Dayton, Ohio, 1975.
40. Heller, H. H., Holmes, D. G., and Covert, E. E., "Flow-induced pressure oscillations in shallow cavities," J. Sound Vib. 18, 545-533(1971).
41. Rossiter, J. E. Wind tunnel experiments in the flow over rectangular cavities at subsonic and transonic speeds. Reps. & Memo. No. 3438. Aeronaut. Res. Counc., London, 1966.
42. Tarn, C. K. W., and Block, Patricia J. W., "On the Tones and Pressure Oscillations Induced by Flow over Rectangular Cavities," J. Fluid Mech., Vol. 89, Part 2, pp. 373-399, 1978.
43. Rockwell, D., and Naudascher, E., "Self-Sustained Oscillations of Impinging Free Shear Layers," Ann. Rev. Fluid Mech., pp. 67-94, 1979.
44. Komerath, N. M., Ahuja, K. K., and Chambers, F. W., "Prediction and Measurement of Flows Over Cavities - A Survey," AIAA 87- 0166, 25th AIAA Aerospace Sciences Meeting, Reno, NV, January 1987., 4 Blake, William, K., Mechanics of Flow-Induced Sound and Vibration, Vol. I - General Concepts and Elementary Sources, Academic Press, Inc., 1986.(see Page 138-149)
45. Hardin, J. C., and Pope, D. S., "Sound Generated by Flow over a Two Dimensional Cavity," AIAA Paper 93-4327, 1993.
46. Colonius, Tim, Basu, Amit J., and Rowley, Clarence W., "Numerical investigation of the flow past a cavity. AIAA-99-1912 (1999).
47. Cain, A.B., Epstein, R. E., and Kerschen, E. J., Quick turnaround prediction of weapons bay cavity acoustics resonance. AIAA-99- 1899, 1999.
48. Ahuja, K. K., and Mendoza, Jeff, "Effects of Caviy Dimensions, Boundary Layer, and Temperature on Cavity Noise with Emphasis on Benchmark Data to Validate Computational Aeroacoustic Codes," NASA CR-4653. February 1995.
49. Rossiter, J. E., "Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds," Ministry of Aviation, Reports and Memoranda No. 3438, October 1964
50. Heller, H., Widnall, S., Jones, J., and Bliss, D., "Water-Table Visualization of Flow-Induced Pressure Oscillations in Shallow Cavities for Simulated Super-sonic Flow Conditions," 86th Meeting of the Acoustical Society of America, Paper Z13, 1973.
51. Shaw, Leonard, and Northcraft, Stephen, "Closed loop active control for cavity acoustics," AIAA-99-1902, 1999.
52. Mendoza, J. M., and Ahuja, K. K., "Cavity Noise Control Through Upstream Mass Injection from a Coanda Surface," AIAA paper 96- 1767, presented at AIAA/CEAS Aeroacoustics Conference, State College, Pennsylvania, May 6-8, 1996.
53. Vakili, A. D., and Gauthier, C., "Control of Cavity Flow by Upstream Mass Injection," Journal of Aircraft, vol. 26, No. 3, pp. 374-376, March 1988.
54. Vakili, Ahmad D., Cooper, Gleen C., and Schatt, Daniel E., "Effect of Upstream Mass Injection Pattern on Cavity Flow Aeroacoustics," Experimental Heat Transfer, Fluid Mechanics, and Thermodynamics 1993, pp. 1154-1164, Jan. Feb. 1994.
55. Lamp, Alison M. and Chokani, Ndaona, Control of cavity resonance using steady and oscillatory blowing. AIAA-99-0999 (1999).
56. Stanek, Michael, J. Sinha, Neeraj, Ahuja, Vineet, and Birkbeck, Roger M., Acoustics compatible active flow control for optimal weapon separation. AIAA-99-1911 (1999).
57. Hsu, J., and Ahuja, K. K., "Cavity Noise Using Helmholtz Resonators," AIAA paper 96-1675, presented at AIAA/CEAS Aeroacoustics Conference, State College, Pennsylvania, May 6-8, 1996. Also,see: Ahuja, K. K., Hsu, J. and Mendoza, J. M., Control of Cavity Noise by Mass Injection, Helmholtz Resonators, and Surface Oscillations, Final Report A9758-000, Prepared for Technology Scientific Services Inc. in support of US Govt. Contract F33491-92-DJ024, November 1995.
58. Raman, Ganesh, Raghu, Surya and Bencic, Timothy J. "Cavity resonance suppression using miniature fluidic oscillators," AIAA-99-1900 1999.
59. Mendoza, J. M. and Ahuja, K. K., "The Effects of Width on Cavity Noise, "CEAS/ AIAA paper 95-054, presented at The First Joint CEAS/AIAA Aeroacoustics Conference (16th AIAA Aeroacoustics Conference), Munich, Germany, June 12-15. 1995.
60. Ahuja, K. K., and Mendoza, Jeff, "Effects of Caviy Dimensions, Boundary Layer, and Temperature on Cavity Noise with Emphasis on Benchmark Data to Validate Computational Aeroacoustic Codes," NASA CR-4653. February 1995.
61. Mendoza, J. M., "Effect of Cavity Dimensions, Boundary Layer, and Temperature on Cavity Noise Generation and Control,: PhD thesis, Georgia Institute of Technology, 1997. Leonard Shaw - Private Communication.
62. Seiner, J. M., "Advances in High Speed Jet Aeroacoustics, AIAA Paper No. 84-2275, 1984.
63. Powell, A., "On the Mechanism of Choked Jet Noise," Proceedings of the Physical Society, Vol. 66, pp. 1039-1056, 1953
64. Davies, M.G. and Oldfield, D.E.S., "Tones from a Choked Axisymmetric Jet," Acustica, Vol. 12, pp. 257-277, 1962.
65. Tam, C.K.W., Seiner, J.M. and Yu, J.C., "Proposed Relationship between Broadband Shock Associated Noise and Screech Tones," Journal of Sound and Vibration, Vol. 110, pp. 309-321, 1986.
66. Shaw, Leonard, and Northcraft, Stephen, "Closed loop active control for cavity acoustics," AIAA-99-1902, 1999.
67. Mendoza, J. M., and Ahuja, K. K., "Cavity Noise Control Through Upstream Mass Injection from a Coanda Surface," AIAA paper 96- 1767, presented at AIAA/CEAS Aeroacoustics Conference, State College, Pennsylvania, May 6-8, 1996.
68. Vakili, A. D., and Gauthier, C., "Control of Cavity Flow by Upstream Mass Injection," Journal of Aircraft, vol. 26, No. 3, pp. 374-376, March 1988.
69. Vakili, Ahmad D., Cooper, Gleen C., and Schatt, Daniel E., "Effect of Upstream Mass Injection Pattern on Cavity Flow Aeroacoustics," Experimental Heat Transfer, Fluid Mechanics, and Thermodynamics 1993, pp. 1154-1164, Jan. Feb. 1994.
70. Lamp, Alison M. and Chokani, Ndaona, Control of cavity resonance using steady and oscillatory blowing. AIAA-99-0999 (1999).
71. Stanek, Michael, J. Sinha, Neeraj, Ahuja, Vineet, and Birkbeck, Roger M., Acoustics compatible active flow control for optimal weapon separation. AIAA-99-1911 (1999).
72. Hsu, J., and Ahuja, K. K., "Cavity Noise Using Helmholtz Resonators," AIAA paper 96-1675, presented at AIAA/CEAS Aeroacoustics Conference, State College, Pennsylvania, May 6-8, 1996. Also,see: Ahuja, K. K., Hsu, J. and Mendoza, J. M., Control of Cavity Noise by Mass Injection, Helmholtz Resonators, and Surface Oscillations, Final Report A9758-000, Prepared for Technology Scientific Services Inc. in support of US Govt. Contract F33491-92-DJ024, November 1995.
73. Raman, Ganesh, Raghu, Surya and Bencic, Timothy J. "Cavity resonance suppression using miniature fluidic oscillators," AIAA-99-1900 1999.
74. Mendoza, J. M. and Ahuja, K. K., "The Effects of Width on Cavity Noise, "CEAS/ AIAA paper 95-054, presented at The First Joint CEAS/AIAA Aeroacoustics Conference (16th AIAA Aeroacoustics Conference), Munich, Germany, June 12-15. 1995.
75. Ahuja, K. K., and Mendoza, Jeff, "Effects of Caviy Dimensions, Boundary Layer, and Temperature on Cavity Noise with Emphasis on Benchmark Data to Validate Computational Aeroacoustic Codes," NASA CR-4653. February 1995.
76. Mendoza, J. M., "Effect of Cavity Dimensions, Boundary Layer, and Temperature on Cavity Noise Generation and Control,: PhD thesis, Georgia Institute of Technology, 1997. Leonard Shaw - Private Communication.
77. Seiner, J. M., "Advances in High Speed Jet Aeroacoustics, AIAA Paper No. 84-2275, 1984.
78. Powell, A., "On the Mechanism of Choked Jet Noise," Proceedings of the Physical Society, Vol. 66, pp. 1039-1056, 1953
79. Davies, M.G. and Oldfield, D.E.S., "Tones from a Choked Axisymmetric Jet," Acustica, Vol. 12, pp. 257-277, 1962.
80. Tam, C.K.W., Seiner, J.M. and Yu, J.C., "Proposed Relationship between Broadband Shock Associated Noise and Screech Tones," Journal of Sound and Vibration, Vol. 110, pp. 309-321, 1986.
81. Raman, G., "Advances in Understanding of Supersonic Jet Noise Screech: Review and Perspective," Progress in Aerospaces Sciences (Including Aircraft Design), Vol. 34, pp. 45-106, 1998. (Also see AIAA Paper 98-0279, 1998.)
82. Ahuja, K. K., "Some Unique Experiments on Receptivity," AIAA 85-0533, AIAA Shear Flow Control Conference, Boulder, CO, March 1985. (Also see Ahuja, K. K., Basic Experimental Study of the Coupling Between Flow Instabilities and Incident Sound, NASA CR-3789, 1984.
83. Ahuja, K. K., Jones, R. R. Ill, Tarn, C. K., Massey, K. C. and Fleming, A. J., "Acoustic Interactions Between an Altitude Test Facility and Jet Engine Plumes: Theory and Experiments," Final Report, AEDC-TR-91-20, Jan. 1992.
84. Massey, Kevin, C., "Flow/Acoustic Coupling in Heated and Unheated Fre and Ducted Jets," PhD Thesis, Georgia Institute of Technology, March 1997.
85. Seiner, J.M. and Norum, T.D. 1979 Experiments of shock associated noise on supersonic jets. AIAA paper 79-1526.
86. Tam, C.K.W. and Hu, F.Q. On the three families of instability waves of high speed jets. Journal of Fluid Mechanics, Vol. 201, pp. 447-483, 1989.
87. Tarn, C. K. W., Ahuja, K. K., and Jones, R. R. III, "Screech Tones From Free and Ducted Supersonic Jets," AIAA Journal; Vol. 32, No. 5, pp.917-922, May, 1994
88. Raman, Ganesh, "Cessation of Screech in Underexpanded Jets." AIAA Paper-96-1719, 1996.
89. Seiner, J.M., Manning J. C., and Ponton, M. K., "Dynamic Pressure Loads associated with of Twin Supersonic Plume Resonance," AIAA Paper 86-1539, 1986.
90. Seiner, J.M., Manning J. C., and Ponton, M. K., "Model and Full- Scale Study of Twin Supersonic Plume Resonance," AIAA Paper 87- 0244, 1987.
91. Norum, T. D., and Shearin, J. G.," Dynamic Loads on Twin Jet Exhaust Nozzles due to Shock Noise,"J. Aircraft, Vol. 23, pp 728-729, 1986.
92. Abdell-Fattah, A.M., and Favalaro, S. C., "Duct Resonance and Its Effect on the Performance of High-Pressure Ratio Axisymetric ejectors," AIAA Journal, Vol. 26, No. 7, July 1988.
93. Jones, R. R. Ill and Lazalier, G. R., "The Acoustic Response of Altitude Test Facility Exhaust Systems to Axisymmetric and Two- Dimensional Turbine Engine Exhaust Plumes," AIAA Paper 92-02- 131, 1992.
94. Ahuja, K. K., Jones, R. R. Ill, Tarn, C. K., Massey, K. C. and Fleming, A. J., "Acoustic Interactions Between an Altitude Test Facility and Jet Engine Plumes: Theory and Experiments," Final Report, AEDC-TR-91-20, Jan. 1992.
95. K. K. Ahuja, K. C. Massey, C. K. W. Tarn, and R. R. Jones, III "Temperature Effects on Acoustic Interactions between Altitude Test Facilities and Jet Engine Plumes," AEDC-TR-94-10, October 1994.
96. Tarn, C. K. W., Ahuja, K. K., and Jones, R. R. III, "Screech Tones From Free and Ducted Supersonic Jets," AIAA Journal; Vol. 32, No. 5, pp.917-922, May, 1994.
97. Jones, R. R. Ill, Ahuja, K. K., Tam, C. K. W., and Abdelwahab, M., "Measured Acoustic Characteristics of Ducted Supersonic Jets at Different Model Scales," AIAA 93-0731, 31st AIAA Aerospace Sciences Meeting and Exhibit, Reno, January 1993.
98. Bruggeman, J. C., Hirschberg, A., van Dongan, M. E. H., Wijnands, A. P. J., and Gorter, J., Self Sustained Aeroacoustic Pulsations in Gas Transport Systems: Experimental Study of the Influence of Closed Side Branches," J. Sound and Vibration, Vol 150 (3), pp 371-393, 1991.
99. Flandro, G. A., "Vortex Driving Mechanism in Oscillatory Rocket Flows," J. Propulsion Vol 2 (3), pp 206-214, 1986.
100. Hourigan, K., Welsh, M. C., Thompson, M. C., and Stokes, A. N., "Aerodynamic Sources of Acoustic Resonance in a duct with Baffles," J. Fluids and Structures, Vol. 4, pp 345-370, 1990
101. Krothapalli. A. Ross, C. Yamamoto, K., "Fuid-Acoustic Interaction in a Low Area Ratio Supersonic Jet Ejector," AIAA-93- 4346, 1993
102. Howe, M. S., "Self-Excited Oscillations in Jet Engine Test Cells," J. Fluid and Structures, Vol. 1, pp. 121-148, 1987.
103. Parker, R., "Resonance in Wake Shedding from Parallel Plates: Some experimental Observations," Journal of Sound and Vibration, Vol. 4, No. 1, pp. 62-67, 1966.
104. Parker, R., "Resonance Effects in Wake Shedding from Parallel Plates: Calculations of Resonant Frequencies," Journal of Sound and Vibration, Vol. 5, No. 2, pp. 332-343, 1967.
105. Parker, R., and Griffiths, W. M., "Low Frequency Resonance Effects in Wake Shedding from Parallel Plates," Journal of Sound and Vibration, Vol. 7, No. 3, pp. 371-379, 1968.
106. Stokes, A. N. and Welsh, M. C., "Flow Resonant Sound Interaction in a Duct Containing a Plate. Part II. Square Leading Edge," Journal of Sound and Vibration, Vol. 192, No. 1, pp. 55-73, 1986.
107. Stonesman, S. A. T., Stokes, A. N. and Welsh, M. C., "Resonant Sound Caused by Flow Past two Plates in Tandem in a Duct Interaction in a Duct Containing a Plate. Part I. Semicircular Leading Edge," Journal of Fluid Mechanics, Vol. 95, pp. 455-484, 1988.
108. Welsh, M. C., Hourigan, K., Welch, L. W., Downie, R. J., Thompson, M. C., and Stokes, A. N., "Acoustics and Experimental Methods: The Influence of Sound on Flow and Heat Transfer," Experimental Thermal and Fluids Science, Vol. 192, No., pp. 138-152, 1990
109. Welsh, M. C., Stokes, A. N., and Parker, R., "Flow Resonant Sound Interaction in a Duct Containing a Plate. Part I. Semicircular Leading Edge," Journal of Sound and Vibration, Vol. 192, No. 3, pp. 305-323, 1984
110. Ahuja, K. K., Manes, J. and Massey, K. C., "Control of Jet Mixing and Supersonic Jet Noise by Resonance Effects in wake Shedding from Parallel Plates," CEAS/AIAA paper 95-018, presented at The First Joint CEAS/AIAA Aeroacoustics Conference (16th AIAA Aeroacoustics Conference), Munich, Germany, June 12-15.
111. Welsh, M. C., Stokes, A. N., and Parker, R., "Flow Resonant Sound Interaction in a Duct Containing a Plate. Part I. Semicircular Leading Edge," Journal of Sound and Vibration, Vol. 192, No. 3, pp. 305-323, 1984
112. Ahuja, K. K., Manes, J. and Massey, K. C., "Control of Jet Mixing and Supersonic Jet Noise by Resonance Effects in wake Shedding from Parallel Plates," CEAS/AIAA paper 95-018, presented at The First Joint CEAS/AIAA Aeroacoustics Conference (16th AIAA Aeroacoustics Conference), Munich, Germany, June 12-15. 1995.
113. Tyndall, J., "Sound," D. Appleton and Co., New York, 1867.
114. Rijke, P. L., "Notiz uber Eine Neue Art, die Luft in Einer an Beiden Enden Offenen Rohre in Schwingunen zu Versetzen," Annalen der Phsik, 107,pp339-343, 1859
115. Rayleigh, J. W. S., "Theory of Sound," New York, Dover Publications, re-issue, Volume 2, 1945.
116. Feldman Jr K. T., "Review of the Literature on Rijke Thermoacoustic Phenomena," J. Sound Vib. Vol 7, No. 1, pp. 83-89, 1968.
117. Cremer, L., and Ising, H., "Die Selbsterregten Schwingungen von Orgelpfeifen,' Acustica, pp 143-153, 167.
118. Coltman, J. W., "Sounding Mechanism of the Flute and Organ Pipe," J. Acoust. Soc.Am, Vol. 44, pp. 983-992, 1968.
119. Coltman, J. W., Acoustics of the of the Flute,.Physics Today, Vol.21 (11), pp. 25-32, 1968.
120. Fletcher, Neville, H. and Rossing, Thomas, D., "The Physics of Musical Instruments." Springer-Verlag New York, Inc., Second Edition, 1998.
121. Olson, Harry F., "Music, Physics, and Engineering," Dover Publications Inc., Second Edition, 1967.
122. Williams, F. A., Barrere, M, and Huang, N. C, "Fundamental Aspects of Solid Propellant Rockets," AGARDograph No. 116, Slough, England, Technivision Services, 1969
123. Williams, F. A., "Combustion Instability,"Addison-Wesley Publishing Company, second Addition, 1985. Rosenberg, L. D. (Editor), Sources of High-Intensity Ultrasound - Volume 1, Plenum Press, 1969
124. Hill, W.G., and Green, P.R., "Increased Turbulent Jet Mixing Rates Obtained by Self-Excited Acoustic Oscillations," ASME Paper No. 77-FE-18, 1977.
125. Yu, K., Gutmark, E., Smith, R. A., and Schadow, K. C., "Supersonic Jet Excitation Using Cavity Forcing," AIAA 94-0185, 1994.
126. Nakazono, Y., Ahuja, K. K., and Mendoza, J. M., "Mixing Enhancement Through Cavity Resonance," AIAA 96-1672, 2nd AIAA/CEAS Aeroacoustics Conference, State College, PA, May 6-8, 1996.