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pro vyhledávání: '"Lakshimi N Sankar"'
Publikováno v:
The Journal of the Acoustical Society of America. 103:644
An active control device for reducing blade-vortex interactions (BVI) noise generated by a rotorcraft, such as a helicopter, comprises a trailing edge flap located near the tip of each of the rotorcraft's rotor blades. The flap may be actuated in any
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6634fde496d3df932f28f715b60b9e48
https://doi.org/10.1121/1.421188
https://doi.org/10.1121/1.421188
