Predictions of the Inlet Splice Effects from the QTD2 Static Test-Reference-Cited by-同舟云学术

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Predictions of the Inlet Splice Effects from the QTD2 Static Test

Published:2007-05-21 Issue: Volume: Page:
ISSN:
Container-title:13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
language:
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Author:

Premo John¹,Breard Cyrille¹,Lan Justin¹

Affiliation:

1. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-3544

Reference10 articles.

1. 2Lan, J.H., Breard, C. "Validation of 3D Acoustic Propagation Code with Analytical and Experimental Results," AIAA 2005-2901.

2. 3Lan,J.H.,Breard,C."DevelopmentandValidationofa3DLinearizedEulerSolver,"AIAA2006-2585.

3. Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics

4. 5Tam,C.K.W.,Hongbin,J.,Chien,E.W."ScatteringofAcousticDuctModesbyAxialLinerSplices,"AIAA2005-2459.

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2. Physical processes influencing acoustic radiation from jet engine inlets;Journal of Fluid Mechanics;2013-05-14

3. Physics of Acoustic Radiation from Jet Engine Inlets;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04

4. The Quiet Technology Demonstrator Program: Static Test of Airplane Noise-Reduction Concepts;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

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