PASSIVE CONTROL OF SHOCK WAVE APPLIED TO HELICOPTER ROTOR HIGH-SPEED IMPULSIVE NOISE REDUCTION
A strong, normal shock wave, terminating a local supersonic area on an airfoil (or a helicopter blade), not only limits the aerodynamic performance, but also becomes a source of High-Speed Impulsive (HSI) noise. The application of a passive control system (a cavity covered by a perforated plate) on...
में बचाया:
| मुख्य लेखकों: | , |
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| स्वरूप: | Artigo |
| भाषा: | Inglês |
| प्रकाशित: |
Gdańsk University of Technology
2010-07-01
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| श्रृंखला: | TASK Quarterly |
| विषय: | |
| ऑनलाइन पहुंच: | https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1999 |
| टैग: |
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