Jet aeroacoustic testing: Issues and implications

AIAA Journal

Volumn 41, Issue 9, 2003, Pages 1674-1679

  Viswanathan, K ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AIRCRAFT MODELS; COMPUTER SIMULATION; JET AIRCRAFT; NOZZLES; PRESSURE;

EFFECTIVE PERCEIVED NOISE LEVEL; JET AEROACOUSTIC TESTS; JET NOISE; NOZZLE PRESSURE RATIOS;

FLIGHT DYNAMICS;

EID: 0141573384     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7313     Document Type: Article

References (11)

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3. Tanna, H. K., "An Experimental Study of Jet Noise. Part I," Journal of Sound and Vibration, Vol. 50, 1977, pp. 405-428.
4. Tanna, H. K., "An Experimental Study of Jet Noise. Part II," Journal of Sound and Vibration, Vol. 50, 1977, pp. 429-444.
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9. Saiyed, N. H., Mikkelsen, K. L., and Bridges, J. E., "Acoustics and Thrust of Separate-Flow Exhaust Nozzles with Mixing Devices for High-Bypass-Ratio Engines," AIAA Paper 2000-1961, June 2000.
10. Kenzakowski, D. C., Shipman, J., Dash, S. M., Bridges, J. E., and Saiyed, N. H., "Turbulence Model Study of Laboratory Jets with Mixing Enhancements for Noise Reduction," AIAA Paper 2000-0219, Jan. 2000.
11. "Gas Turbine Jet Exhaust Noise Prediction," Society of Automotive Engineers, Paper SAE ARP876, Rev. D, Jan. 1994.