Predictions of the inlet splice effects from the QTD2 static test

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

Volumn , Issue , 2007, Pages

  Premo, John ^a   Breard, Cyrille ^a   Lan, Justin ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOEING COMPANIES; FULL SCALE TESTS; HIGH QUALITY; IMPEDANCE DISCONTINUITIES; NOISE MEASUREMENTS; PREDICTION PROCESS; QUIET TECHNOLOGY DEMONSTRATOR 2; STATIC TESTS;

ACOUSTIC NOISE MEASUREMENT; AEROACOUSTICS; FORECASTING; SCATTERING;

ACOUSTIC NOISE;

EID: 78249239741     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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5. Tam, C.K.W., Hongbin, J., Chien, E. W., "Scattering of Acoustic Duct Modes by Axial Liner Splices, " AIAA 2005-2459.
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7. Yu, J., Nesbitt, E., Kwan, H., Uellenberg, S., Chien, E., Premo, J., "Quiet Technology Demonstrator 2 Intake Liner Design and Validation, " AIAA-2006-2458.
8. Callender, B., Janardan B., Uellenberg S., Premo J., Kwan, H.W., Abeysinghe, A., "QTD2 Static Test-Acoustic Benefits of a Smooth Inlet, " AIAA-2007-3671.
9. W. Bi, V. Pagneux, D. Lafarge, and Y. Aurégan, "Characteristics of penalty mode scattering by rigid splices in lined ducts", AIAA-2005-2897.
10. D.C. Pridmore-Brown, "Sound propagation in a fluid flowing through an attenuating duct", Journal of fluid mechanics, 4:393-406, 1958.