Waves Transmission and Generation in Turbine Stages in a Combustion-Noise Framework-Reference-Cited by-同舟云学术

Waves Transmission and Generation in Turbine Stages in a Combustion-Noise Framework

Published:2010-06-07 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Leyko Mateusz¹,Moreau Stephane²,Nicoud Franck³,Poinsot Thierry⁴

Affiliation:

1. CERFACS

2. University of Sherbrooke

3. University Montpellier II

4. IMF Toulouse

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4032

Reference18 articles.

1. 1Candel, S., Analytical studies of some acoustic problems of jet engines., Ph.D. thesis,California Institute of Technology, Pasadena, California, 1972.

2. Comparison of Direct and Indirect Combustion Noise Mechanisms in a Model Combustor

3. The application of a semi-actuator disk model to sound transmission calculations in turbomachinery, part I: The single blade row

4. The application of a semi-actuator disk model to sound transmission calculations in turbomachinery, part II: Multiple blade rows

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