Validation of Acoustic Propagation Code with JT15D Static and Flight Test Data-Reference-Cited by-同舟云学术

Validation of Acoustic Propagation Code with JT15D Static and Flight Test Data

Published:2004-05-10 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/CEAS Aeroacoustics Conference
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Author:

Lan Justin¹,Guo Yueping¹,Breard Cyrille²

Affiliation:

1. The Boeing Company

2. Analytical Methods Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2986

Reference13 articles.

1. 1Lan, J. H., Guo, Y., and Breard, C. "Validation and Application of Two Frequency Domain Acoustic Propagation Codes," AIAA 2003-3244.

2. 2Heidmann,M.F.,Saule,A.V.,andMcArdle,J.G."AnalysisofRadiationPatternsofInteractionTonesGeneratedby Inlet Rods in the JT15D Engine," AIAA 79-0581.

3. 3McArdle,J.G.,Jones,W.L.,Heidelberg,L.J.,andHomyak,L."Comparisonof SeveralInflowControlDevicesforFlight Simulation ofFan Tone Noise Using a JT15D-1 Engine," AIAA 80-1025.

4. 4Heidelberg, L. J., Rice, E. J., and Homyak, L. "Acoustic Performance of Inlet Suppressors on an Engine Generating a Single Mode," NASA TM-82697 or AIAA 81-1965.

5. Finite Element-Integral Acoustic Simulation of JT15D Turbofan Engine

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