Airframe Noise Prediction Using Navier-Stokes Code with Cartesian and Boundary-fitted Layer Meshes-Reference-Cited by-同舟云学术

Airframe Noise Prediction Using Navier-Stokes Code with Cartesian and Boundary-fitted Layer Meshes

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
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Author:

Ueno Yosuke¹,Ochi Akio¹

Affiliation:

1. Kawasaki Heavy Industries, Ltd.

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. 1Nagata,T., Ueno, Y., and Ochi, A. "Validation of new CFD tool usingNon-orthogonal Octree with Boundary-fitted Layer UnstructuredGrid,"AIAAPaper 2012-1259,2012.

2. TAS Code, FaSTAR, and Cflow Results for the Sixth Drag Prediction Workshop

3. 3Hashimoto,A.,Aoyama,T.,Matsuo,Y.,Ueno,M.,Nakakita,K.,Hamamoto,S.,Sawada,K.,Matsushima,K.,Imamura,T., Ochi,A.,andYoshimoto, M."Summaryof FirstAerodynamicsPredictionChallenge(APC-I),"AIAAPaper 2016-1780,2016.

4. 4Yasuda, H., Nagata, T., Ueno, Y., and Ochi, A. "Prediction of Aerodynamic Characteristics Using CFD on the Aircraft High-LiftConfiguration," APISAT,Toyama,2016.

5. 5Ito, Y., Murayama, M., Yokokawa, Y., Yamamoto, K., Tanaka, K., Hirai, T., Yasuda, H., Tajima, A., and Ochi, A."Japan Aerospace Exploration Agency's and Kawasaki Heavy Industries' Contribution to the Third High Lift Prediction Workshop," AIAAPaper2018-1034,2018.

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