[1] |
POWELL A. On the noise emanating from a two-dimensional jet above the critical pressure[J]. Aeronautical Quarterly, 1953, 4(2):103-122.
|
[2] |
TAM C K W, AURIAULT L.Jet mixing noise from fine-scale turbulence[J]. AIAA Journal, 1999, 37(2):145-153.
|
[3] |
汪海洋, 李晓东. 超声速喷流啸声的控制方法[J]. 推进技术, 2007, 28(2):211-215. WANG H Y, LI X D. Control methods for supersonic jet screech tones[J]. Journal of Propulsion Technology, 2007, 28(2):211-215(in Chinese).
|
[4] |
BRIDGES J, WERNET M P. Turbulence measurements of rectangular nozzles with bevel:AIAA-2015-0228[R]. Reston, VA:AIAA, 2015.
|
[5] |
MUNRO S E, AHUJA K K. Aeroacoustics of a high aspect-ratio jet:AIAA-2003-3323[R]. Reston, VA:AIAA, 2003.
|
[6] |
BRIDGES J. Acoustic measurements of rectangular nozzles with bevel:NASA/TM-2012-217674[R]. Washington, D.C.:NASA, 2012.
|
[7] |
TAM C K W, ZAMAN K M. Subsonic jet noise from non-axisymmetric and tabbed nozzles[J]. AIAA Journal, 2000, 38(4):592-599.
|
[8] |
PALIATH U, MORRIS P J. Prediction of jet noise from rectangular nozzles:AIAA-2006-0618[R]. Reston, VA:AIAA, 2006.
|
[9] |
HROMISIN S M, AKATSUKA J, MCLAUGHLIN D K, et al. Aeroacoustic performance of multi-stream, rectangular, supersonic jets:AIAA-2019-1301[R]. Reston, VA:AIAA, 2019.
|
[10] |
CRAWLEY M, FISCHER M K, SAMIMY M. Control of a supersonic rectangular jet using plasma actuators:AIAA-2012-2211[R]. Reston, VA:AIAA, 2012.
|
[11] |
MASSEY K C, AHUJ K K, GAETA R. Noise scaling for unheated low aspect ratio rectangular jets:AIAA-2004-2946[R]. Reston, VA:AIAA, 2004.
|
[12] |
WESTLEY R, WOOLLEY J H. An investigation of the near noise fields of a choked axisymmetric air jet[C]//Proceedings of AFOSR-UTIAS Symposium on Aerodynamic Noise. Toronto:University of Toronto Press, 1968:147-167.
|
[13] |
AHUJA K, TESTER B, TANNA H. Calculation of farfield jet noise spectra from near field measurements with true source location[J]. Journal of Sound and Vibration, 1987, 116(3):415-426.
|
[14] |
NICK P B, AHUJA K K. Subsonic jet noise source location as a function of nozzle geometry:AIAA-2019-0250[R]. Reston, VA:AIAA, 2019.
|
[15] |
LAUFER J, SCHLINKER R, KAPLAN R E. Experiments on supersonic jet noise[J]. AIAA Journal, 1976, 14(4):489-497.
|
[16] |
FISHER M J, HARPER B M, GLEGG S. Jet engine noise source location:The polar correlation technique[J]. Journal of Sound and Vibration, 1977, 51(1):23-54.
|
[17] |
WATTS M E, MOSHER M, BARNES M J. The microphone array phased processing system(MAPPS):AIAA-1996-1714[R]. Reston, VA:AIAA, 1996.
|
[18] |
PODBOY G G, BRIDGES J E, HENDERSON B S. Phased array noise source localization measurements of an F404 nozzle plume at both full and model scale:GT2010-22601[R]. New York:ASME, 2010.
|
[19] |
VENKATESH S, POLAK D, NARAYANAN S. Phased array design, validation, and application to jet noise source localization:AIAA-2000-1934[R]. Reston, VA:AIAA, 2000.
|
[20] |
LEE S S, BRIDGES J. Phased-array measurements of single flow hot jets:AIAA-2005-2842[R]. Reston, VA:AIAA, 2005.
|
[21] |
TESTER B J, GLEGG S A L. A review of engine noise source diagnostic methods for static engine tests, with phased array and polar correlation techniques:AIAA-2008-2854[R]. Reston, VA:AIAA, 2008.
|
[22] |
JAMES P E, PRAVEEN P, PATRICK V, et al. Acoustic source localization of rectangular jets using large eddy simulation with numerical phased arrays:AIAA-2014-0179[R]. Reston, VA:AIAA, 2014.
|
[23] |
SIMONICH J C, NARAYANAN S, SCHLINKER R H. Facility and data quality issues for scale-model jet noise testing:AIAA-2003-1057[R]. Reston, VA:AIAA, 2003.
|
[24] |
SAE. Standard values of atmospheric absorption as a function of temperature and humidity:SAE Standard ARP866A[S]. New York:SAE, 1975.
|
[25] |
THOMAS J M. Aeroacoustic measurements[M]. Berlin:Springer, 2002:109-117.
|