Effect of cross-section on flow three-dimensionality for prismatic bodies and the associated noise emission
Author:
Affiliation:
1. Institut Pprime
Publisher
American Institute of Aeronautics and Astronautics
Reference71 articles.
1. 446 0.170-0.214 2.7 0.484 0.222-0.276
2. × 10(AR =1) 1.3 [37, 38] 1.15-1.71†
3. 392-0.481 2.7 0.372-0.446
4. × 20(AR =2) 1.3 [16, 37, 39, 40] 0.83-1.36†
5. 099-0.153 2.7 0.111-0.182
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