The Quiet Technology Demonstrator program: Static test of an Acoustically Smooth Inlet

13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)

Volumn , Issue , 2007, Pages

  Callender, Bryan ^a   Janardan, Bangalore ^a   Uellenberg, Stefan ^b   Premo, John ^b   Kwan, Hwa Wan ^c   Abeysinghe, Amal ^c  

^a GE AVIATION   (United States)

^b BOEING COMPANY   (United States)

^c GOODRICH CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CABIN NOISE; DESIGN FEATURES; FLIGHT TEST PROGRAMS; MULTIPLE PURE TONES; NOISE REDUCTION TECHNOLOGIES; PRODUCTION DESIGNS; QUIET TECHNOLOGY DEMONSTRATORS; STATIC TESTS;

AEROACOUSTICS; DESIGN; NOISE ABATEMENT; SOFTWARE TESTING;

ACOUSTIC NOISE;

EID: 84884776531     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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2. Ganz, U. W., Strout, F. G., "Evaluation of High Fan Tone Noise Levels in Static Testing, " Boeing Internal Paper NOIS-B8310-C86-229RES, October 24, 1986.
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11. Gantie, F., Batard, H., Baker, N., and Schwaller, P., "Zero Splice Intake Technology and Acoustic Benefits", AIAA-2006-2455, Cambridge, MA, 2006.
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13. Tam, C., Ju, H., Chin, E., "Scattering of Acoustic Duct Modes by Axial Liner Splices", AIAA-2006-2459, Cambridge, MA, 2006.