The Fast Random Particle Method for Combustion Noise Prediction
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2451
Reference42 articles.
1. Numerical analysis of the acoustic field of reacting flows via acoustic perturbation equations
2. Evaluation of the RPM Approach for the Simulation of Broadband Combustion Noise
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