Acoustic and Flow-Field Measurements of a Long Duct Chevron Mixer-Reference-Cited by-同舟云学术

Acoustic and Flow-Field Measurements of a Long Duct Chevron Mixer

Published:2007-05-21 Issue: Volume: Page:
ISSN:
Container-title:13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
language:
Short-container-title:

Author:

Wojno John¹,Martens Steven²,Bridges James³,Brown Clifford³

Affiliation:

1. General Electric Aviation

2. General Electric Global Research Center

3. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-3600

Reference22 articles.

1. 3Salikuddin, M., Babbit, R., Shin, H., Wisler, S., Janardan, B., and Majjigi, R. "Acoustic and Laser Doppler Anemometer Results for Confluent and 12-Lobed E3MixerExhaustSystemsforSubsonicJetNoiseReduction,"NASA CR-2002-211597,2002.

2. 4Salikuddin, M., Martens, S., Shin, H., and Majjigi, R. "Acoustic and Laser Doppler Anemometer Results for Confluent, 22-Lobed, and Unique Lobed Mixer Exhaust Systems for Subsonic Jet Noise Reduction," NASA CR-2002-211598,2002.

3. 5Janardan, B., Hoff, G., Barter, J., Martens, S., and Gliebe, P. "AST Critical Propulsion and Noise Reduction Technologies for Future Commercial Subsonic Engines, Separate Flow Exhaust System Noise Reduction Concept Evaluation,"NASA CR-2000-210039, 2000.

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