Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Amal Abeysinghe"'
Autor:
Ronen Elkoby, Jefferey W. Moe, Mehdi R. Khorrami, Amal Abeysinghe, Robert W. Stoker, Leon Brusniak
Publikováno v:
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference).
With continued growth in air travel, sensitivity to community noise intensifies and materializes in the form of increased monitoring, regulations, and restrictions. Accordingly, realization of quieter aircraft is imperative, albeit only achievable wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::93c2b04012eede9b8cd9a48c2583c4c5
https://doi.org/10.2514/6.2007-3457
https://doi.org/10.2514/6.2007-3457
Autor:
Hwa-Wan Kwan, Bryan Callender, Amal Abeysinghe, Bangalore Janardan, John Premo, Stefan Uellenberg
Publikováno v:
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference).
The QTD2 static engine test sought to provide further insight into the noise reduction technologies demonstrated during the 2005 flight test program. One of the technologies demonstrated in the QTD2 program was the Acoustically Smooth Inlet. This tec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1dfd003c4cac6e8f0b836585e8b02da9
https://doi.org/10.2514/6.2007-3671
https://doi.org/10.2514/6.2007-3671
Publikováno v:
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference).
The advances in aircraft engine noise reduction and the increasing demand for quieter aircraft has led noise research to focus more attention on airframe noise. Landing gears and high lift systems have been known to significantly contribute to the to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e73764a48872cc0aace1a108ab76c4a
https://doi.org/10.2514/6.2007-3456
https://doi.org/10.2514/6.2007-3456
Publikováno v:
12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference).
Fluidic chevrons use injected air near the trailing edge of a nozzle to emulate mixing and jet noise reduction characteristics of mechanical chevrons. While previous investigations of "first generation" fluidic chevron nozzles showed only marginal im
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e0c549219dd9beda3af4de6b456d3d4
https://doi.org/10.2514/6.2006-2706
https://doi.org/10.2514/6.2006-2706
Publikováno v:
11th AIAA/CEAS Aeroacoustics Conference.
The impact of alternating fluidic core chevrons on the production of jet noise is investigated. Core nozzles for a representative 1/9th scale, bypass ratio 5 model system were manufactured with slots cut near the trailing edges to allow for air injec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2241bd2bea3d37c6195989efa7a61a0e
https://doi.org/10.2514/6.2005-2888
https://doi.org/10.2514/6.2005-2888