Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Leon Brusniak"'
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::28fb0483c70bbdc8bd8acc21f60131c6
https://doi.org/10.2514/6.2021-2162
https://doi.org/10.2514/6.2021-2162
Publikováno v:
International Journal of Aeroacoustics. 16:326-357
Detailed acoustic measurements of the noise from the leading-edge Krueger flap of a 5.75% hybrid wing body aircraft model were acquired with a traversing phased microphone array in the Arnold Engineering Development Complex NFAC 40- by 80-foot wind t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::414f3d791a683ee8f89b6cdc09f66363
https://doi.org/10.1177/1475472x17719104
https://doi.org/10.1177/1475472x17719104
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Acoustic phased array flyover noise measurements were acquired as part of the Boeing 737 MAX-7 NASA Advanced Inlet Liner segment of the Quiet Technology Demonstrator 3 (QTD3) flight test program. This paper reports on the processes used for separatin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f10c9c043bab9807dbc83f54f8be86f
https://doi.org/10.2514/6.2019-2765
https://doi.org/10.2514/6.2019-2765
Publikováno v:
AIAA Journal. 51:2935-2945
This paper presents an analysis of the slat noise for hybrid wing–body aircraft. It is shown that the hybrid wing–body slat noise is characterized by its broad spectral shapes with frequencies depending on both the mean flow velocity and the airc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75629194c86fe39fb63c9f6715bb2961
https://doi.org/10.2514/1.j052540
https://doi.org/10.2514/1.j052540
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Detailed acoustic measurements of the noise from the leading-edge Krueger flap of a 5.75% Hybrid Wing Body (HWB) aircraft model were recently acquired with a traversing phased microphone array in the AEDC NFAC 40by 80-Foot Wind Tunnel at NASA Ames Re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c7f9b3d648e6f944fd58e62cc3892802
https://doi.org/10.2514/6.2016-0012
https://doi.org/10.2514/6.2016-0012
Publikováno v:
AIAA Journal. 49:1577-1599
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ad79485b34b2f9d98ae6255b148b9dc2
https://doi.org/10.2514/1.j050750
https://doi.org/10.2514/1.j050750
Autor:
Leon Brusniak, David S. Dolling
Publikováno v:
Journal of Fluid Mechanics. 273:375-409
Fluctuating wall-pressure measurements have been made on the centreline upstream of a blunt fin in a Mach 5 turbulent boundary layer. By examining the ensemble-averaged wall-pressure distributions for different separation shock foot positions, it has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57cf146abed9250f29f6a6b948e31329
https://doi.org/10.1017/s0022112094001989
https://doi.org/10.1017/s0022112094001989
Publikováno v:
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference).
Jet-flap interaction (JFI) noise can become an important component of far field noise when a flap is immersed in the engine propulsive stream or is in its entrained region, as in approach conditions for under-the-wing engine configurations. We experi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a825a1c5143eb15d73d6b078e9809eb1
https://doi.org/10.2514/6.2007-3666
https://doi.org/10.2514/6.2007-3666
Publikováno v:
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc7016ec987df7f4cd87b338e54a1026
https://doi.org/10.2514/6.2007-3612
https://doi.org/10.2514/6.2007-3612
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