Hybrid Empirical/Computational Aeroacoustics Methodology for Rocket Noise Modeling
Author:
Affiliation:
1. Italian Aerospace Research Center, I-81043 Capua, Italy
2. European Launch Vehicle, S.p.A., I-00034 Colleferro, Italy
3. Avio S.p.A., I-00034 Colleferro, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.38634
Reference29 articles.
1. Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
2. Impact of Subgrid-Scale Models on Jet Turbulence and Noise
3. Sound generation in a mixing layer
4. Computation of Flow Noise Using Source Terms in Linearized Euler's Equations
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