Compressor Noise Contribution to Inlet Noise
- Author(s):
- Agarwal, N. ( The Boeing Co, Seattle,WA )
- Ganz, U.
- Premo, J.
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA/CEAS Aeroacoustics Conference
- Ser. no.:
- 10th
- Pub. Year:
- 2004
- No.:
- 2004-2913
- Paper no.:
- AIAA-2004-2913
- Pub. info.:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200408 [CD-ROM 2004 Disc 8]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
The Quiet Technology Demonstrator Program: Static Test of an Acoustically Smooth Inlet
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Fan Noise Source Diagonostic Test - Wall Measured Circumferential Array Mode Results
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Measurement and Prediction of the Tonal Noise of a Centrifugal Compressor at Inlet
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |