Direct simulation of acoustic scattering by a rotorcraft fuselage-Reference-Cited by-同舟云学术

Direct simulation of acoustic scattering by a rotorcraft fuselage

Published:2000-06-12 Issue: Volume: Page:
ISSN:
Container-title:6th Aeroacoustics Conference and Exhibit
language:
Short-container-title:

Author:

Agarwal Anurag¹,Morris Philip¹

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2030

Reference16 articles.

1. 1Chung, C., Wave Propagation and Scattering In Computational Aeroacoustics, PhD dissertation,The Pennsylvania State University, Departmentof Aerospace Engineering,Apr. 1995.

2. Acoustic Scattering from Two- and Three-Dimensional Bodies

3. Direct Simulation of Acoustic Scattering by Two- and Three-Dimensional Bodies

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

5. An efficient and robust method for predicting helicopter rotor high-speed impulsive noise

Cited by 6 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. Boundary element analysis on the fuselage scattering of drone noise;International Journal of Aeroacoustics;2022-02-26

2. Computational Aeroacoustics;Unsteady Computational Fluid Dynamics in Aeronautics;2014

3. A Brinkman penalization method for compressible flows in complex geometries;Journal of Computational Physics;2007-12

4. Radiation and Wall Boundary Conditions for Computational Aeroacoustics: A Review;International Journal of Computational Fluid Dynamics;2004-08

5. Simulation of Shockwave - Structure Interaction with the Brinkman Penalization Method;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05