R. Westley and G. M. Lilley, 1952, "An investigation of the noise field from a small jet and methods for its reduction", Report No. 53, College of Aeronautics, Cranfield, England.
	Harper-Bourne, M. and Fisher, M. J., "The noise from shock waves in supersonic jets", Proc. on Noise Mechanisms, AGARD CP-131, 1973, pp. 11-1 to 11-13.
	Tanna, H. K., "An experimental study of Jet Noise, Part II: Shock Associated Noise", J. Sound and Vib., 50, Feb. 1977, pp. 429-444. CrossRef
	Seiner, J. M. and Yu, J. C., 1981, "Acoustic near field and local flow properties associated with broadband shock noise", AIAA Paper-81-1975, 7th Aeroacoustics Conf., Palo Alto, CA, October 5-7.
	Norum, T. D., 1983, "Screech suppression in supersonic jets", AIAA J., 21(2), pp. 235-240. CrossRef
	Nagel, R. T., Denham, J. W. and Papathanasiou, A. G., 1983, "Supersonic jet screech tone cancellation", AIAA J., 21(11), pp. 1541-1545. CrossRef
	Westley, R., 2003, "A tribute to Alan Powell and a search for jet screech source simplification," Int. J. of Aeroacoustics, 2(3), pp. 219-224. Abstract
	Paterson, R. W., Vogt, P. G. and Foley, W. M., 1972, "Design and development of the United Aircraft Research Laboratories acoustic research tunnel", AIAA Paper 72-1005, AIAA 7th Aerodynamic Testing Conf., Palo Alto, CA, Sept. 13-15.
	Long, M. J., 1992, "Experimental Investigation of an Ejector-Powered Free-Jet Facility," NASA TM-105868.
	Castner, R. A., 1994, "The Nozzle Acoustic Test Rig; an acoustic and aerodynamic free-jet facility", AIAA Paper 94-2565, 18th AIAA Aerospace Ground Testing Conf., Colorado Springs, CO, June 20-23.
	Bradbury L. J. S. and Khadem A. H., 1975, "The distortion of a Jet by Tabs", J. Fluid Mech., 70, 801-813. CrossRef
	Pannu, S. S. and Johannesen, N. H., 1976, "The structure of jets from notched nozzles", J. Fluid Mechanics, 74(3), pp. 515-528. CrossRef
	Ahuja K. K. and Brown W. H., 1989, "Shear flow control by mechanical tabs", AIAA Paper No. 89-0994.
	Brown, W. H. and Ahuja, K. K., 1989, "Shear flow control of cold and heated rectangular jets by mechanical tabs", NASA CP-182296.
	Zaman, K. B. M. Q., Reeder, M. F. & Samimy, M., 1992, "Supersonic jet mixing enhancement by ‘delta tabs’", AIAA paper 92-3548, 28th Joint Prop. Conf., Nashville, TN.
	Samimy, M., Zaman, K. B. M. Q. & Reeder, M. F. 1993, "Effect of tabs on the flow and noise field of an axisymmetric jet," AIAA J. 4, 1251-1258.
	Zaman, K. B. M. Q., Reeder, M. F. & Samimy, M., 1994, "Control of an axisymmetric using vortex generators", Phys. Fluids 6, 778-793.
	Reeder, M. F. and Zaman, K. B. M. Q., 1996, "The impact of tab location relative to the nozzle exit on jet distortion", AIAA J., 34, pp.197-199. CrossRef
	Foss, J. K. & Zaman, K. B. M. Q., 1999, "Large- and small-scale vortical motions in a shear layer perturbed by tabs", J. Fluid. Mech. 382, 307-329. CrossRef
	Kim, J.-H. and Samimy, M., 1999, "Mixing enhancement via nozzle trailing edge modifications in high speed rectangular jet", Phys. Of Fluids, 11(9), pp. 2731-2742. CrossRef
	Reeder, MF. & Samimy, M., 1996, "The evolution of a jet with vortex-generating tabs: real-time visualization and quantitative measurements", J. Fluid Mech., 311, pp. 73-118. CrossRef
	Bohl, D. & Foss, J. F., 1997, "An experimental study of the near field region of a free jet with passive mixing tabs," NASA CR-97-206296.
	Bohl, D. & Foss, J. F., 1999, "Near exit plane effects caused by primary and primary-plus-secondary tabs," AIAA J., 37(2), 192-201. CrossRef
	Foss, J. K. & Zaman, K. B. M. Q., 1996, "Effect of delta tab on fine-scale mixing in a turbulent two-stream shear layer", AIAA Paper 96-0546.
	Naughton J., Cattafesta, L. and Settles, G., 1989, "An experimental study of the effect of streamwise vorticity on supersonic mixing enhancement", AIAA Paper 89-2456, 25th Joint Propulsion Conf., Monterey, CA, July 10-12.
	Carletti, M., Rogers, C. B. and Parekh, D. E., 1993, "The use of streamwise vorticity to enhance ejector performance", AIAA Paper 93-3247, Shear Flow Conf., Orlando, FL., July 6-9.
	Rogers, C. B. and Parekh, D. E., 1994, "Mixing enhancement by and noise characteristics of streamwise vortices in an air jet", AIAA J., 32(3), pp. 464-471. CrossRef
	Ahuja, K. K., Manes, J. P. and Calloway, A. B., 1990, "An evaluation of various concepts of reducing supersonic jet noise", AIAA Paper 90-3982, 13th Aeroacoustics Conf., Tallahassee, FL., Oct. 22-24.
	Ahuja, K. K., 1993, "Mixing enhancement and jet noise reduction through tabs plus ejectors", AIAA Paper 93-4347, 15th Aeroacoustics Conf., Long Beach, CA, Oct. 25-27.
	Zhang, S. & Schneider, S. P., 1995, "Quantitative molecular-mixing measurements in a round jet with tabs", Phys. Fluids 7, 1063-1070. CrossRef
	Sujith, R. I., Ramesh, R., Pradeep, S., Sriram, S. and Muruganandum, T. M., 2001, "Mixing of high speed coaxial jets", Exp. Fluids, 30, pp. 339-345. CrossRef
	Yu, S. C. M., Koh, P. K. and Chua L. P., 2001, "An experimental investigation of two-stream mixing flow with a single delta tab", Int. J. of Heat and Fluid Flow, 22, pp. 62-71. CrossRef
	Verma, S. B. and Rathakrishnan, E., 2001, "Experimental study on the flow and noise characteristics of underexpanded notched slot jets", The Aeronautical J., May, pp. 267-275.
	Seiner, J. M. and Grosch, C. E., 1998, "Mixing enhancement by tabs in round supersonic jets", AIAA Paper 98-2326, 4th AIAA/CEAS Aeroacoustics Conf., Toulouse, France, June 2-4.
	Steffen, C. J., Reddy, D. R. and Zaman, K. B. M. Q., 1997, "Numerical modeling of jet entrainment for nozzles fitted with delta tabs", AIAA Paper 97-0709, Aerospace Sciences Meeting, Reno, NV, January.
	Saiyed, N. H. and Bridges, J. E., 1999, "Tabs and mixers for reducing low bypass ratio jet noise", AIAA Paper 99-1986, 5th AIAA/CEAS Aeroacoustics Conf., Bellevue, Washington.
	Low, J. K.C, Schweiger, P. S., Premo, J. W. and Barber, T. J., 2000, "Advanced Subsonic Technology (AST) Separate-Flow High-Bypass Ratio Nozzle Noise Reduction Program Test Report," NASA CR 2000-210040.
	Janardan, B. A., Hoff, G. E., Barter, J. W., Martens, S., Gliebe, P. R., Mengle, V. and Dalton, W. N., 2000, "AST Critical Propulsion and Noise Reduction Technologies for Future Commercial Subsonic Engines Separate-Flow Exhaust System Noise Reduction Concept Evaluation," NASA CR 2000-210039.
	Brausch, J. F., Bangalore, A. J., Barter, J. W. and Hoff, G. E., 2002, "Chevron exhaust nozzle for gas turbine engine", US patent 6360528 B1.
	Saiyed, N. H., editor, 2000, "Separate Flow Nozzle Test Status Meeting," NASA CP 2000-210524.
	Saiyed, N., Mikkelsen, K. L., and Bridges, J., 2000, "Acoustics and Thrust of Separate-Flow Exhaust Nozzles With Mixing Devices for High-Bypass-Ratio Engines," NASA TM 2000-209948.
	Callendar, B., Gutmark, E. and Martens, S., 2005, "Far-field acoustic investigation into chevron nozzle mechanisms and trends", AIAA J., 43(1), pp. 87-95. CrossRef
	Callendar, B., Gutmark, E. and Martens, S., 2008, "Near-field investigation of chevron mechanisms", AIAA J., 46(1), pp. 36-44. CrossRef
	Bridges J. E., & Wernet, M., 2002, "Turbulence measurements of separate flow nozzles with mixing enhancement features", AIAA Paper 2002-2484.
	Bridges, J. E., Wernet, M. and Brown, C. A., 2003, "Control of jet noise through mixing enhancement", Noise-Con, Cleveland, Ohio, June 23-25, (NASA TM 2003- 212335).]
	Zaman, K. B. M. Q., Wang, F. Y. and Georgiadis, N. J., 2003, "Noise, turbulence and thrust of subsonic free jets from lobed nozzles", AIAA J., 41(3), pp. 398-407. CrossRef
	Reba, R., Simonich, J. and Schlinker, R., 2008, "Measurement of source wave-packet in highspeed jets and connection to far-field sound", AIAA Paper 2008-2891, 14th AIAA/CEAS Aeroacoustics Conf., Vancouver, Canada, May 5-7.
	Reba, R., Simonich, J. and Schlinker, R., 2009, "Sound radiated by large-scale wave-packets in subsonic and supersonic jets", AIAA Paper 2009-3256, 15th AIAA/CEAS Aeroacoustics Conf., Miami, FL, May 11-13.
	Suzuki, T. and Colonius, T., 2006, "Instability waves in a subsonic round jet detected using a nearfield phased microphone array", J. Fluid Mechanics, 565:197-226 CrossRef
	Kenzakowski, D. C., Shipman, J., Dash, S. M., Bridges, J. E. and Saiyed, N. H., 2000, "Study of three-stream laboratory jets with passive mixing enhancements for noise reduction", AIAA Paper 2000-0219, 38th Aerospace Sciences Meeting, Jan. 10-13, Reno, NV.
	Koch, L. D., Bridges, J. E. and Khavaran, A., 2004, "Mean flow and noise prediction for a separate flow jet with chevron mixers", AIAA Paper 2004-0189, 42nd Aerospace Sciences Meeting, Reno, NV, Jan. 5-8.
	Engblom, W. A., Khavaran, A. and Bridges, J. E., 2004, "Numerical prediction of chevron nozzle noise reduction using WIND-MGBK methodology", AIAA paper 2007-3596, 13th AIAA/CEAS Aeroacoustics Conf., Rome, Italy.
	Birch, S. F., Lyubimov, D. A., Maslov, V. P. and Secundov, A. N., 2006, "Noise prediction for chevron nozzle flows", AIAA paper 2006-2600, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Gudmundsson, K. and Colonius, T., "Spatial stability analysis of chevron jet profiles", AIAA Paper 2007-3599, 13th AIAA/CEAS Aeroacoustics Conference, May, Rome, Italy.
	Shur, M. L., Spalart, P. R., Strelets, M. K. and Garbaruk, A. V., 2007, "Analysis of jet-noise-reduction concepts by large-eddy simulation", Int. J. of Aeroacoustics, 6(3), pp. 243-285. Abstract
	Kailasanath, K., Liu, J., Gutmark, E., Munday, D. and Mertens, S., 2009, "Impact of mechanical chevrons on supersonic jet flow and noise", Proc. ASME Turbo Expo., GT2009, June 8-12, Orlando, FL.
	Turner, T. L., Cabell, R. H., Cano, R. J. and Silcox, R. J., 2008, "Development of a preliminary model-scale adaptive jet engine chevron", AIAA J., 46(10), pp. 2545-2557. CrossRef
	Uzun, A. and Hussaini, Y., 2009, "Simulation of noise generation in the near-nozzle region of a chevron nozzle jet", AIAA J., 47(8), pp. 1793-1810. CrossRef
	Karabasov, S. A., Hao, X., Graham, O., Hynes, T. P., Tucker, P. G. and Dowling, A. P., 2010, "Low-order modeling for chevron jet noise based on LES data", AIAA Paper 2010-3964, 16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden.
	Xia, H., Tucker, P. G. and Eastwood, S., 2009, "Large-eddy simulations of chevron jet flows with noise predictions", Int. J. of Heat and Fluid Flow, 30(6), pp. 1067-1079. CrossRef
	Tide, P. S. and Srinivasan, K., 2010, "Effect of chevron count and penetration on the acoustic characteristics of chevron nozzles", Applied Acoustics, 71(3), pp. 201-220. CrossRef
	Weir, D. S., 2004, "Engine validation of noise reduction concepts - separate flow nozzles", AIAA Paper 2004-188, 42nd Aerospcae Sciences Meeting, Reno, NV, 5-8 January.
	Brown, C. A. and Bridges, J. E., 2003, "An Analysis of Model Scale Data Transformation to Full Scale Flight Using Chevron Nozzles", NASA TM 2003-212732.
	Herkes, W. H., Olsen, R. F. and Ullenberg, S., 2006, "The Quiet Technology Demonstrator program: flight validation of airplane noise-reduction concepts", AIAA Paper 2006-2720, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Mengle, V. G., Elkoby, R., Brusniak, L. and Thomas, R. H., 2006, "Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 1. Isolated nozzles", AIAA Paper 2006-2467, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Mengle, V. G., Elkoby, R., Brusniak, L. and Thomas, R. H., 2006, "Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 2. Installed nozzles", AIAA Paper 2006-2434, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Mengle, V. G., Elkoby, R., Brusniak, L. and Thomas, R. H., 2006, "Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 3. Jet-flap interactions", AIAA Paper 2006-2435, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Mengle, V. G., Ganz, U. W., Nesbitt, E., Bultemeier, E. J., and Thomas, R. H., 2006, "Flight test results for uniquely tailored propulsion-airframe aeroacoustic chevrons: shockcell noise", AIAA Paper 2006-2439, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Nesbitt, E., Mengle, V. G., Czech, M. and Thomas, R. H., 2006, "Flight test results for uniquely tailored propulsion-airframe aeroacoustic chevrons: community noise", AIAA Paper 2006-2439, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.
	Calkins, F. T., Butler, G. and Mabe, J. H., 2006, "Variable geometry chevrons for jet noise reduction," AIAA Paper 2006-2546, 12th AIAA/CEAS Aeroacoustics Conf., Cambridge, MA, May 8-10.