The Development of the Ducted Fan Noise Propagation and Radiation Code CDUCT-LaRC-Reference-Cited by-同舟云学术

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The Development of the Ducted Fan Noise Propagation and Radiation Code CDUCT-LaRC

Published:2003-05-12 Issue: Volume: Page:
ISSN:
Container-title:9th AIAA/CEAS Aeroacoustics Conference and Exhibit
language:
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Author:

Nark Douglas¹,Farassat Fereidoun¹,Pope D. Stuart²,Vatsa Veer¹

Affiliation:

1. NASA Langley Research Center

2. Analytical Services & Materials

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3242

Reference6 articles.

1. Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces

2. On the acoustic boundary condition in the presence of flow

3. A SIMPLE DERIVATION OF THE ACOUSTIC BOUNDARY CONDITION IN THE PRESENCE OF FLOW

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2. Bypass Duct Acoustic Liner Design With and Without Bifurcation Effects;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

3. Multi-degree-of-freedom liner development: Concept to flight test;International Journal of Aeroacoustics;2021-06-28

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5. Review on ducted fans for compound rotorcraft;The Aeronautical Journal;2020-01-16

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