Prediction of Noise from Realistic Rotor-Wake / Stator-Row Interaction Using Computational Aeroacoustics

Prediction of Noise from Realistic Rotor-Wake / Stator-Row Interaction Using Computational Aeroacoustics

著者名:

Hixon, Ray ( University of Toledo, Toledo, Ohio, 43606, USA )
Sescu, Adrian ( University of Toledo, Toledo, Ohio, 43606, USA )
Nallasamy, M. ( ASRC Aerospace, Kennedy Space Center, FL 32899, USA )
Sawyer, Scott ( University of Akron, Akron, Ohio 44325, USA )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

シリーズ巻号:

2009

発行年:

2009

通号:

2009-3339

ペーパー番号:

AIAA Paper 2009-3339

総ページ数:

3

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200906

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00066596
シリーズID:	PA00000149
会議名:	AIAA/CEAS Aeroacoustics Conference
回次:	15
会議開催地:	Miami, Florida
会議開催年:	2009.05.11-2009.05.13
論文注記:	DOI:10.2514/6.2009-3339 // 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) 11 - 13 May 2009, Miami, Florida

類似資料:

1 テクニカルペーパー Computational Aeroacoustic Prediction of Discrete-Frequency Noise Generated by a Rotor-Stator Interaction Sawyer, S., Nallasamy, M., Hixon, R., Dyson, R., Koch, D. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Parallelization Strategy for an Explicit Computational Aeroacoustics Code Hixon, R., Nallasamy, M., Sawyer, S. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Validation of a CAA Code Using a Benchmark Wake-Stator Interaction Problem Sescu, Adrian, Hixon, Ray, Sawyer, Scott American Institute of Aeronautics and Astronautics	8 テクニカルペーパー High-Accuracy Large-Step Explicit Runge-Kutta (HALE-RK) Schemes for Computational Aeroacoustics R. Hixon, V. Allampali, M. Nallasamy, S. Sawyer American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Modal Decomposition of Rotor Wake-Stator Interaction Noise in a Swirling Shear Flow S. Sawyer, M. Nallasamy, R. Hixon American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Mean Flow Boundary Conditions for Computational Aeroacoustics Hixon, R., Nallasamy, M., Sawyer, S., Dyson, R. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー The Influence of Steady Loading on Discrete-Frequency Rotor-Stator Interaction Noise Sawyer, S., Nallasamy, M., Hixon, R., Dyson, R.W. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Shock-Capturing Dissipation Schemes for High-Accuracy Computational Aeroacoustics (CAA) Codes R. Hixon, D. Bhate, M. Nallasamy, S. Sawyer American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Comparison of Numerical Schemes for a Realistic Computational Aeroacoustics Benchmark Problem Hixon, R., Nallasamy, M., Sawyer, S., Dyson, R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Unsteady Validation of a Mean Flow Boundary Condition for Computational Aeroacoustics Hixon,R., Nallasamy,M., Sawyer,S., Dyson,R. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Validation of a Computational Aeroacoustics Code for Nonlinear Flow about Complex Geometries Using Ringleb's Flow Satav, V., Hixon, R., Nallasamy, M., Sawyer, S. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー A Time Domain Analysis of Gust-Cascade Interaction Noise Nallasamy, M., Hixon, R., Sawyer, S., Dyson, R., Koch, L. American Institute of Aeronautics and Astronautics

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