Aircraft System Noise Shielding Prediction with a Kirchhoff Integral Method-Reference-Cited by-同舟云学术

Aircraft System Noise Shielding Prediction with a Kirchhoff Integral Method

Published:2017-06-02 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA/CEAS Aeroacoustics Conference
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Author:

Guo Yueping¹,Pope Dennis S.²,Burley Casey L.³,Thomas Russell H.³

Affiliation:

1. NEAT Consulting

2. Analytical Mechanics Associates, Inc.

3. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3196

Reference28 articles.

1. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments

2. Propulsion Airframe Aeroacoustic Integration Effects for a Hybrid Wing Body Aircraft Configuration

3. Bonet, J. T., Schellenger, H. G., Rawdon, B. K., Elmer, K. R., Wakayama, S. R., Brown, D., and Guo, Y. P. "Environmentally Responsible Aviation (ERA) Project - N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV), Final Report," NASA Contract Report 2013-216519, 2013.

4. Guo, Y. P., Nickol, C. L., and Thomas, R. H. "Noise and Fuel Burn Reduction Potential of an Innovative Subsonic Transport Configuration," AIAA Paper 2014-0257.

5. Guo, Y. P., Burley, C. L., and Thomas, R. H. "On Noise Assessment for Blended Wing Body (BWB) Aircraft," AIAA Paper 2014-0365.

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