The use of a rotating Kirchhoff formulation for high-speed impulsive noise-Reference-Cited by-同舟云学术

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The use of a rotating Kirchhoff formulation for high-speed impulsive noise

Published:1994-01-10 Issue: Volume: Page:
ISSN:
Container-title:32nd Aerospace Sciences Meeting and Exhibit
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Author:

Lyrintzis A.¹,Xue Y.¹,Kilaras M.¹

Affiliation:

1. Minnesota Univ., Minneapolis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-463

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Integrated Aero-Acoustic Rotor Simulation and Design Optimization;12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference);2006-05-08

2. Surface Integral Methods in Computational Aeroacoustics—From the (CFD) Near-Field to the (Acoustic) Far-Field;International Journal of Aeroacoustics;2003-04

3. PREDICTION AND VALIDATION ON THE SONIC BOOM BY A HIGH-SPEED TRAIN ENTERING A TUNNEL;Journal of Sound and Vibration;2001-10

4. Rotorcraft impulsive noise prediction using a rotating Kirchhoff formulation;Journal of Aircraft;1996-11

5. Towards a versatile Kirchhoff code for aeroacoustic predictions;Aeroacoustics Conference;1996-05-06

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